EP2852990B1 - Multifunctional cell for structural applications - Google Patents

Multifunctional cell for structural applications Download PDF

Info

Publication number
EP2852990B1
EP2852990B1 EP13795889.8A EP13795889A EP2852990B1 EP 2852990 B1 EP2852990 B1 EP 2852990B1 EP 13795889 A EP13795889 A EP 13795889A EP 2852990 B1 EP2852990 B1 EP 2852990B1
Authority
EP
European Patent Office
Prior art keywords
separator
electrochemical device
anode
cathode
current collectors
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP13795889.8A
Other languages
German (de)
French (fr)
Other versions
EP2852990A2 (en
Inventor
Jay R. Sayre
Steven M. Risser
Andrew James Manning
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Battelle Memorial Institute Inc
Original Assignee
Battelle Memorial Institute Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Battelle Memorial Institute Inc filed Critical Battelle Memorial Institute Inc
Publication of EP2852990A2 publication Critical patent/EP2852990A2/en
Application granted granted Critical
Publication of EP2852990B1 publication Critical patent/EP2852990B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/50Current conducting connections for cells or batteries
    • H01M50/543Terminals
    • H01M50/545Terminals formed by the casing of the cells
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01GCAPACITORS; CAPACITORS, RECTIFIERS, DETECTORS, SWITCHING DEVICES OR LIGHT-SENSITIVE DEVICES, OF THE ELECTROLYTIC TYPE
    • H01G11/00Hybrid capacitors, i.e. capacitors having different positive and negative electrodes; Electric double-layer [EDL] capacitors; Processes for the manufacture thereof or of parts thereof
    • H01G11/52Separators
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01GCAPACITORS; CAPACITORS, RECTIFIERS, DETECTORS, SWITCHING DEVICES OR LIGHT-SENSITIVE DEVICES, OF THE ELECTROLYTIC TYPE
    • H01G11/00Hybrid capacitors, i.e. capacitors having different positive and negative electrodes; Electric double-layer [EDL] capacitors; Processes for the manufacture thereof or of parts thereof
    • H01G11/66Current collectors
    • H01G11/72Current collectors specially adapted for integration in multiple or stacked hybrid or EDL capacitors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01GCAPACITORS; CAPACITORS, RECTIFIERS, DETECTORS, SWITCHING DEVICES OR LIGHT-SENSITIVE DEVICES, OF THE ELECTROLYTIC TYPE
    • H01G11/00Hybrid capacitors, i.e. capacitors having different positive and negative electrodes; Electric double-layer [EDL] capacitors; Processes for the manufacture thereof or of parts thereof
    • H01G11/74Terminals, e.g. extensions of current collectors
    • H01G11/76Terminals, e.g. extensions of current collectors specially adapted for integration in multiple or stacked hybrid or EDL capacitors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01GCAPACITORS; CAPACITORS, RECTIFIERS, DETECTORS, SWITCHING DEVICES OR LIGHT-SENSITIVE DEVICES, OF THE ELECTROLYTIC TYPE
    • H01G11/00Hybrid capacitors, i.e. capacitors having different positive and negative electrodes; Electric double-layer [EDL] capacitors; Processes for the manufacture thereof or of parts thereof
    • H01G11/78Cases; Housings; Encapsulations; Mountings
    • H01G11/80Gaskets; Sealings
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01GCAPACITORS; CAPACITORS, RECTIFIERS, DETECTORS, SWITCHING DEVICES OR LIGHT-SENSITIVE DEVICES, OF THE ELECTROLYTIC TYPE
    • H01G11/00Hybrid capacitors, i.e. capacitors having different positive and negative electrodes; Electric double-layer [EDL] capacitors; Processes for the manufacture thereof or of parts thereof
    • H01G11/78Cases; Housings; Encapsulations; Mountings
    • H01G11/82Fixing or assembling a capacitive element in a housing, e.g. mounting electrodes, current collectors or terminals in containers or encapsulations
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/04Construction or manufacture in general
    • H01M10/0413Large-sized flat cells or batteries for motive or stationary systems with plate-like electrodes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/04Construction or manufacture in general
    • H01M10/0436Small-sized flat cells or batteries for portable equipment
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/05Accumulators with non-aqueous electrolyte
    • H01M10/052Li-accumulators
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/05Accumulators with non-aqueous electrolyte
    • H01M10/052Li-accumulators
    • H01M10/0525Rocking-chair batteries, i.e. batteries with lithium insertion or intercalation in both electrodes; Lithium-ion batteries
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/05Accumulators with non-aqueous electrolyte
    • H01M10/058Construction or manufacture
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/06Lead-acid accumulators
    • H01M10/12Construction or manufacture
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • H01M50/102Primary casings, jackets or wrappings of a single cell or a single battery characterised by their shape or physical structure
    • H01M50/103Primary casings, jackets or wrappings of a single cell or a single battery characterised by their shape or physical structure prismatic or rectangular
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • H01M50/102Primary casings, jackets or wrappings of a single cell or a single battery characterised by their shape or physical structure
    • H01M50/105Pouches or flexible bags
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • H01M50/116Primary casings, jackets or wrappings of a single cell or a single battery characterised by the material
    • H01M50/117Inorganic material
    • H01M50/119Metals
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • H01M50/183Sealing members
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • H01M50/183Sealing members
    • H01M50/186Sealing members characterised by the disposition of the sealing members
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10Primary casings, jackets or wrappings of a single cell or a single battery
    • H01M50/183Sealing members
    • H01M50/19Sealing members characterised by the material
    • H01M50/193Organic material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/411Organic material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/411Organic material
    • H01M50/414Synthetic resins, e.g. thermoplastics or thermosetting resins
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/411Organic material
    • H01M50/414Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/417Polyolefins
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/411Organic material
    • H01M50/414Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/423Polyamide resins
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/411Organic material
    • H01M50/414Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/426Fluorocarbon polymers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/46Separators, membranes or diaphragms characterised by their combination with electrodes
    • H01M50/461Separators, membranes or diaphragms characterised by their combination with electrodes with adhesive layers between electrodes and separators
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/489Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/50Current conducting connections for cells or batteries
    • H01M50/531Electrode connections inside a battery casing
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2220/00Batteries for particular applications
    • H01M2220/20Batteries in motive systems, e.g. vehicle, ship, plane
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/13Energy storage using capacitors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/49108Electric battery cell making
    • Y10T29/49112Electric battery cell making including laminating of indefinite length material

Definitions

  • batteries serve multiple purposes.
  • the lead acid batteries in forklifts serve as ballast for stability.
  • batteries there are however, more instances where added weight and or volume are not beneficial.
  • engineers would like to get electrochemical devices to provide additional functions besides power.
  • multi-functional composites containing energy storage would find application.
  • batteries take up space, one of the most obvious approaches is to have them contribute to the mechanical aspects of the structure. As most batteries are delivered in cases, it is technically feasible to try to gain structural aspects from fastening them together. However, this after-the-fact approach is not optimal.
  • Unmanned Arial Vehicles UAVs
  • Micro UAVs that have electric propulsion are excellent examples which are critically dependent on weight and where composite structural panels are common. Accordingly, there is interest in using advanced multi-functional composites. Bending modulus is critical to UAV panels and the mechanics of bending are well understood. Consumer electronics are additional examples that are dependent on mass and volume. Accordingly, it is desirable to use multi-functional cells in the structure of these devices to reduce the mass and volume associated with the power supply without reducing the capacity or safety.
  • WO 2010/062391 A2 pertains to a high energy density bicell battery being constructed from positive and negative electrodes, with a layer separating the two electrodes, and polymer packaging heat-sealed around the electrode assemblies.
  • a galvanic cell that comprises thin electrodes sealed in plastic foils which are partly metallized on sides forming an electrical contact with the electrode on one side and an external flag on the other side.
  • US 2010/190047 A1 discloses a stacked energy storage device having at least two cell segments arranged in a stack. In particular, each cell segment has a first electrode unit having a first active material electrode, a second electrode unit having a second active material electrode, and an electrolyte layer between the active material electrodes.
  • JP 2007 066806 A pertains to a bipolar battery that has a single cell comprising a cathode active layer, an electrolyte layer and an anode active layer. The single cell is arranged between a pair of current collectors and a flexible armoring material in which a sealing part is arranged to seal the single cell.
  • An electrochemical device comprises one or more anode, cathode, and separator. In addition it has two or more current collectors.
  • the separator is also an electrolyte.
  • the anode and cathode are between the two current collectors and each is adhered to an adjacent current collector.
  • the separator is between the anode and cathode and adhered to the anode and cathode.
  • the current collectors are a barrier, and are sealed together to create a sealed container for the anode, cathode, and separator.
  • the electrochemical device may be integrated into a composite or polymer panel suitable for uses such as structural load bearing panels or sheets for aircraft wings or fuselage, composite armor, unmanned underwater vehicle, torpedo, missile body, consumer electronics, etc.
  • the electrochemical device may include, but is not limited to, energy storage (batteries, supercapacitors), and energy generation (fuel cells).
  • the storage device is: thinner, lighter with higher energy, power, or both per unit mass and volume (specific energy and density), can conform to a variety of surface shapes, and can withstand mechanical loads.
  • the device may be a battery, supercapacitor, a combination of both, or other electrochemical device.
  • a multilayer electrochemical device embedded within a composite or polymer panel possesses both the mechanical attributes necessary to carry shear stress, thus contributing to the bending modulus and increased energy density for any given chemistry.
  • the electrochemical device may use various battery chemistries or super capacitor chemistries.
  • Panels containing these devices can be made with various three dimensional structures which can provide structural support. Thin structures can withstand some degree of flexing.
  • the devices may be used in a variety of structural panels subjected to stresses for many applications.
  • the outside layer metal current collectors act as the packaging for the electrochemical device, and all the inner layers of the electrochemical device, including the current collectors, the anode(s) and cathode(s) and the separator(s) are adhered together so as not to provide a slip plane that would compromise the strength of the panel.
  • An electrochemical device (10) comprises one or more anode (11), cathode (12), and separator (13).
  • the separator (13) is also an electrolyte.
  • it has two or more current collectors (14).
  • the anode (11) and cathode (12) are between the two current collectors (14) and each is adhered to an adjacent current collector (14).
  • the separator (13) is between the anode (11) and cathode (12) and adhered to the anode (11) and cathode (11).
  • the current collectors (14) are a barrier against leakage of the electrolyte and against moisture and oxygen.
  • the device (10) additionally comprises a perimeter seal (15).
  • the perimeter seal (15) is bonded between the two outer current collectors (14), and the combination of outer current collectors (14) and perimeter seal (15) act to create the sealed container for the one or more anode (11), cathode (12), and separator (13).
  • the electrochemical device comprises two or more anodes, cathodes, or both.
  • the anodes or cathodes may be double-sided, which is an electrode attached to a current collector, such as in the middle of the electrode layer.
  • a separator layer is on both sides of the double-sided electrode, and the opposite electrode is adjacent to the separator layer on both sides.
  • the device comprises at least one double-sided cathode. In some embodiments, the device comprises at least one double-sided anode.
  • the anode may be for a lithium ion electrochemical device.
  • anodes include, but are not limited to carbon, lithium titanate, silicon, tin, and others.
  • the anode should be pin hole free.
  • the anode may be for a NiMH (nickel metal hydride) electrochemical device.
  • NiMH nickel metal hydride
  • anodes include, but are not limited to hydrogen-absorbing metal alloys.
  • the anode may be for a supercapacitor.
  • Examples of anodes include, but are not limited to high surface area carbon, metal oxides, and nitrides.
  • the anode may be for a lead acid electrochemical device.
  • anodes include, but are not limited to lead, lead compounds such as lead sulfate, carbon, and lead-carbon mixtures.
  • the anode may be for a Li-S (lithium sulfur) electrochemical device.
  • Other anodes are well known in the art.
  • the thickness of the anode is from about anode 1 to about 100 microns, such as about 10 to about 80 microns, about 20 to about 70 microns, about 25 to about 60 microns, and about 20 to about 40 microns.
  • the cathode may be for a lithium ion electrochemical device.
  • cathodes include, but are not limited to lithium cobalt oxide, nickel cobalt aluminum oxide, manganese oxide, manganese spinel, nickel-manganese-cobalt oxide, nickel-manganese oxide, lithium iron phosphate, lithium cobalt phosphate, lithium manganese phosphate, and derivatives, and sulfur.
  • the cathode may be for a NiMH (nickel metal hydride) electrochemical device.
  • NiMH nickel metal hydride
  • cathodes include, but are not limited to nickel hydroxyl and oxyhydroxy compounds.
  • the cathode may be for a supercapacitor.
  • cathodes examples include, but are not limited to high surface area carbon, metal oxides, and nitrides.
  • the supercapacitor cathode has the same composition as the anode, or may have a different composition.
  • the cathode may be for a lead acid electrochemical device.
  • examples of cathodes include, but are not limited to lead sulfate, and lead oxide.
  • the cathode may be for a Li-S (lithium sulfur) electrochemical device. Other cathodes are well known in the art.
  • the thickness of the cathode is from about 1 to about 200 microns, such as about 10 to about 150 microns, about 25 to about 120 microns, and about 50 to about 100 microns, and about 60 to about 80 microns.
  • the current collector may be for an anode or cathode.
  • the outer current collectors act as a barrier, which prevents the passage of electrolyte, oxygen and water. In some embodiments, the current collector acts as a mass transport barrier. Examples of current collectors for anodes include copper, aluminum, nickel, and stainless steel. Aluminum current collectors may be useful for both the anode and cathode if the cell voltage is about 3 volts or less.
  • the outer current collectors are a solid foil and of sufficient thickness so as not to have pinholes. In some embodiments, the outer current collectors are very thin, such as about 5 to about 50 microns, about 10 to about 30 microns, about 10 to about 25 microns, or about 15 to about 20 microns.
  • the inner current collectors are very thin, such as about 5 to about 50 microns, about 10 to about 30 microns, about 10 to about 25 microns, or about 15 to about 20 microns.
  • the current collectors are electrochemically stable to the voltages of the cell and preferably exhibit low resistance. They are of sufficient strength to be processed and preferably can bend around rolls for continuous processing.
  • the external current collectors are pinhole free to provide the barrier properties and of at least minimal strength to prevent damage during processing and integration into a composite. The surface should provide good wetting and bonding to the resin of the composite. Examples of current collectors for cathodes include aluminum and stainless steel. In some embodiments, the current collector may be nickel.
  • a current collector may be embedded within an anode or cathode (double-sided anode or cathode) if it is not the outer layer of the electrochemical device.
  • a current collector within an anode or cathode need not be a solid foil, it may selected from expanded metals, carbon nonwoven webs, and metal coated carbon non-woven webs and metal coated non-woven polymer webs.
  • all the cathodes are electrically connected together in parallel, such as by connecting all the current collectors attached to the cathodes, and all the anodes are electrically connected together in parallel, such as by connecting all the current collectors attached to the anodes.
  • the electrodes are connected serially.
  • the outer current collectors are bonded or adhered to the adjacent electrode. In some embodiments, the outer current collectors are each independently bonded or adhered to anodes. In some embodiments, the outer current collectors are each independently bonded or adhered to cathodes.
  • the outer current collectors are prepared by one of several methods.
  • the electrode material may be "patch" coated onto the current collector. Patch coating involves applying coating to only a portion of the current collector, such as leaving the perimeter clean so that the perimeter may be sealed to the other outer current collector. Patch coating can be achieved by intermittent coating by a reverse roll or similar coater, a screen coater/printer, printing, gravure coating, ink jet printing, or any other application technique that permits uncoated areas.
  • Another method is to apply a continuous coating and then clean off the areas to seal.
  • a third way is to mask the area to be left uncoated. It may be beneficial to use a primer between the current collector and the electrode to increase adhesion and/or improve performance as is well known in the art.
  • the outer current collectors can be welded together. They are fully welded together with the exception of a passage for the alternate terminal. This can be accomplished by ultrasonic welding, laser welding, or a pulsed DC welder with a contact wheel known as a rotary seamer.
  • the outer current collectors provide a very good barrier. They are sealed hermetically. However, even when sealed, the current collectors allow the opposite electrode to exit the device without making an electrical connection to the opposite electrode.
  • the electrochemical device additionally comprises a perimeter seal.
  • the perimeter seal is also a barrier to oxygen, or moisture, and a barrier to the electrolyte.
  • the perimeter seal is used as an electrical insulator to prevent an electrical connection between the two outer current collectors.
  • the perimeter seal is stable in the presence of the electrolytes and may help to carry stress.
  • the current collector may be treated beforehand to enhance the sealing to the perimeter seal.
  • perimeter seals include: ionomer resins (such as Surlyn®), ethylene acrylic acid (EAA), polyolefin, acidified polyolefin, polyvinylidene difluoride (PVDF), polyimide, polyamide, epoxy, and polyurethane, and other polymeric material that bonds well to metal foils and is inert to the electrolyte.
  • the separator is bonded to the perimeter seal.
  • a perimeter seal is bonded to the outer current collectors, and acts as a barrier to moisture, oxygen, or both, and prevents the migration of the electrolyte. Transmission through the seal is dependent upon the seal width and cross-section. A thinner and/or wider seal minimizes migration.
  • the films prior to sealing are in the range of about 10 to about 150 microns, such as about 25 to about 125 microns, about 30 to about 110 microns, or about 50 to about 100 microns.
  • the perimeter seal is applied as a coating.
  • the perimeter seal is able to withstand the buildup of internal pressure (up to about 2 atmospheres) and temperatures of at least 130°C.
  • the separator is an electrical insulator that allows the electrolyte to conduct ions without conducting electrons.
  • the separator is also an electrolyte.
  • an adhesive layer is applied to the separator to adhere the anode and the cathode to the separator.
  • separators include microporous polyolefin, a ceramic coated polyethylene terephthalate (PET), and PVDF.
  • the separator is coated with an adhesive layer selected from poly(vinylidene fluoride-co-hexafluoropropylene) (PVDF-HFP) copolymer, chlorinated polypropylene, and maleic anhydride/polypropylene.
  • the separator is a polymer selected from polyimides and polyamides, wherein the polymer is interdispersed with at least one adhesive resin, such as modified polypropylene, to form a separator with intrinsic adhesive characteristics.
  • the separator is a polymer selected from crosslinked PVDF and crosslinked poly(ethylene oxide) (PEO).
  • the adhesive layers are thermally activated, the adhesive is activated, and the separator bonds the electrodes together after the electrolyte has been added and allowed to migrate into the separator and electrodes.
  • a low melting point adhesive resin such as about 80 to about 85[deg.]C
  • the separator is from about 5 to about 250 microns in thickness, such as from about 10 to about 100 microns, and about 10 to about 50 microns.
  • the separator has void space.
  • the separator is from about 10% to about 90% void, such as from about 20% to about 80%), about 30% to about 80%, about 40% to about 70%, and from about 45%) to about 65%>.
  • the voids in the separator are in the form of interconnected pores.
  • the average size of the pores in the separator range from about 30 nm to 10 microns, such as from about 40 nm to about 7 microns, about 50 nm to about 5 microns, and from about 100 nm to about 2 microns.
  • the separator (13) is wrapped around an electrode and sealed around it.
  • the separator (13) is effectively formed into a bag or pouch like structure and an electrode is enclosed inside the separator (13), as shown in Figure 2 .
  • the outer current collectors (14) are sealed together to form a perimeter seal (15). This helps to prevent shorting.
  • the electrode is double-sided. When the device is fabricated, an electrode enclosed in a separator (13) is placed on top of an electrode of the opposite polarity, and a second electrode of the opposite polarity is placed on top of the enclosed electrode.
  • the electrolyte used in the electrochemical device depends on the nature of the anode and cathode.
  • the electrolyte may be a liquid or solid.
  • the electrolyte may be a mixture of carbonates or other high dielectric solvents with a lithium containing salt, such as L1CO3, LiPF 6, LiAs 4, LiB0 4, lithium bis(oxalate)borate (LiBOB), and triflate.
  • solvents examples include ethylene carbonate (EC), diethyl carbonate (DEC), dimethyl carbonate (DMC), ethylmethyl carbonate (EMC), propylene carbonate (PC), [gamma]-butyrolactone, as well as special additives such as vinyl ethylene carbonate (VEC), fluoro ethylene carbonate (FEC), and methyl acetate (MA).
  • EC ethylene carbonate
  • DEC diethyl carbonate
  • DMC dimethyl carbonate
  • EMC ethylmethyl carbonate
  • PC propylene carbonate
  • VEC vinyl ethylene carbonate
  • FEC fluoro ethylene carbonate
  • MA methyl acetate
  • concentration of the salts is optimized to the system, but is generally in the range of 1 molar.
  • the electrolyte may be an ionic liquid.
  • the electrolyte may be an aqueous alkaline solution, such as potassium hydroxide.
  • the electrolyte is an aqueous acidic solution
  • electrochemical device may also comprise a supercapacitor.
  • the electrolyte may be either an aqueous or nonaqueous solvent containing a salt or other ionic species.
  • a structural panel may be made comprising the electrochemical device.
  • the panel and the electrochemical device provide a structural support. Because the electrochemical device is a solid mass and can transmit stress and does not compress or slip it does not weaken or significantly weaken the panel it is part of.
  • the electrochemical device can then be assembled into panels by embedding one or more in a mosaic structure as shown in Figure 3 , within a composite.
  • the composite comprises a thin glass fiber (or other suitable material) / epoxy (or other suitable material) layer on each side.
  • the composite adhesively bonds to the outer current collector metal surfaces of the electrochemical device and provides protection to the outer current collectors.
  • the cells can easily be arranged and wired in series connections to provide conventional voltages of 14V, 28V, or even higher voltages within a single panel.
  • the mosaic structure offers further benefits of creating a honeycomb like continuous phase.
  • the size of the electrochemical devices can be adjusted to optimize different objectives. Very large electrochemical devices can be used to maximize specific energy, or a mosaic of smaller cells can be used to provide redundancy in case an electrochemical device is damaged (by enemy fire or other events).
  • the panel is planar, or has a simple (single directional) curve. It can be thin or ultrathin which provides a much higher specific energy for the form factor. This structural integrity is a necessary element of producing a curved cell that will retain its shape. Using the outside current collector layer metals as the packaging of the cell eliminates the non-contributing weight of the pouch packaging.
  • the panel material becomes the battery package, which bonds to the metal surfaces of the foils during processing and protects the cells from physical damage.
  • the panel material is a composite selected from carbon fiber and fiberglass.
  • the majority of the outer surface of the electrochemical device is encased in the polymer. In some embodiments, the electrochemical device and panel are curved.
  • the individual electrochemical devices may be laid up as a two-dimensional tiled array within the composite.
  • the gaps between the single electrochemical devices of a multi-cell battery will also allow for adhesive bonding between successive layers of composite materials, or will allow the polymeric panel material to fill the gaps.
  • the design can employ large numbers of individual electrochemical devices in parallel and in series to provide higher total capacity as well as higher voltages. Further the multi-electrochemical device two-dimensional array design provides a high level of redundancy where if one electrochemical device is damaged, the remainder of the electrochemical devices will still function.
  • the layers in the electrochemical device are fully bonded rather than a stack of loose individual layers.
  • Outer packaging is not needed for the electrochemical device; instead the current collectors serve as part or all of the packaging, as shown in the cell design of Figure 4 and the image of Figure 5 .
  • the electrochemical device as it is a laminated structure, can be easily fabricated in a simple curved structure as well a flat panel.
  • the device must have the appropriate dimensions for the curvature and must be fabricated in or near the final shape. Complex contours are possible by pre-forming the foils.
  • the outer current collector forms one terminal, which may be either copper or aluminum foil, may have a tab for the opposite electrode coming though the sealed outer current collectors, or the perimeter seal on one side.
  • the device can be structured with copper foil on one side and aluminum (positive terminal) on the other.
  • the cells can then be assembled into panels by embedding them in a composite or polymer with a thin composite or resin layer on each side as shown in Figures 3 and 4 .
  • the electrochemical device may be incorporated into a variety of fabrication methods, such as hand layup, resin transfer molding, vacuum assisted resin transfer molding, resin film infusion, filament winding, pultrusion, etc., thereby creating complex 3D multifunctional structures (including sandwich constructions, which combine a lightweight core material with laminated composite skins). Adhesion of the electrochemical device within the panel prevents it from behaving as a defect or a void by allowing the matrix to bond to the metal foils.
  • the outer current collectors are treated before cell assembly to enhance the adhesion between the resin and the current collector. Methods to enhance adhesion include mechanically or chemically roughening the outer surface of the current collectors to increase surface area, or applying a tie coating such as a silane to the outer surface of the current collector.
  • This composite integrates structural and energy functionality into a single component to eliminate the redundancies of parasitic mass that previously existed in the sum of the individual components.
  • the result is a multifunctional composite panel that produces a 39% or greater increase in specific energy compared to standard batteries containing the same chemistry, and offers an opportunity to increase payload, operational lifetime, safety, or function compared to state-of-the art battery technologies.
  • the electrochemical device is a Li-ion bi-cell that comprises a bonded microporous polymeric separator, copper foil current collectors (about 10 microns thick), aluminum foil current collectors (about 15 microns thick), and liquid EC/EMC electrolyte.
  • the electrochemical device has two outside anodes and a double-sided cathode.
  • Such an electrochemical device may be 0.33 mm thick, have a nominal open circuit voltage of 3.7 V per cell, and a 5.6 mAh/cm 2 cathode capacity (2.8mAh/cm 2 per side). Assuming a 100 cm 2 cell active area, this equates to a 560 mAh cell capacity producing 2.072 Wh at a mass of 11 g.
  • the specific energy is 188.72 Wh/kg
  • the areal energy density is 207.2 Wh/m 2 .
  • the result would be total energy storage of 2,072 Wh for a vehicle.
  • the gain in specific energy for this size device is significant.
  • a conventional cell and packaging of this scale weights approximately 4 g more, which means the specific energy would drop to approximately 136 Wh/kg.
  • the electrochemical device has an approximately 39% improvement in specific energy over a state-of-the-art Li-ion cell, assuming one could be procured at 0.33 mm thickness.
  • the electrochemical devices may be fabricated into a composite at either 95°C or 130°C.
  • An upper limit of 130°C allows this technology to be embedded into ultra high molecular weight polyethylene (UHMWPE), such as Dyneema® and Spectra Shield®, or fiberglass composites, such as HJ1, during consolidation.
  • UHMWPE ultra high molecular weight polyethylene
  • the Freya Energy safety separator (developed by Freya Energy Inc, Melbourne FL, www.freyaenergy.com to provide improved safety in lithium ion cells), was modified by Freya Energy by increasing the percentage bonding resin and changing the thermal protection resin to increase the adhesive bond strength and increase the temperature tolerance for the composite fabrication. Processing pressures are not an issue for the cells as they are designed to withstand 68947 kPa (10,000 psi) hydrostatic pressure; therefore, they should withstand typical composite processing pressures.
  • an electrochemical device has multiple electrodes, which together to give a thicker, higher capacity, and higher specific energy device. This is especially useful where the bending modulus is more important than strength (such as in an airfoil) as the thicker device adds thickness to the composite panel.
  • a thicker device also facilitates the use of non-woven current collectors in the inner electrodes further increasing specific energy and energy density.
  • the electrochemical device is a supercapacitor, or a battery hybridized with a supercapacitor.
  • a supercapacitor device that has an anode and cathode material with overall density of about 2g/cm 3
  • the electrolyte has a density of about 1g/cm 3
  • the anode and cathode material will have a capacitance of about 200F/g
  • the capacitance of the system is about 0.2F (because the electrodes are in series).
  • a vehicle has usable surface area of 10 m 2 , then there can be a total energy storage of 6.25 Wh due to the supercapacitor alone, for a single layer device with a thickness 70 microns. If multiple layers are formed, the areal energy density will increase. With 20 layers (approaching 1mm thick), the energy density would be 12.5 Wh/m 2 .
  • Table 1 shows a breakdown of the attributes of an electrochemical battery and supercapacitor.
  • composite materials can offer a multitude of other properties such as good vibrational damping and low coefficient of thermal expansion. These characteristics may be modified to allow them to be engineered for specialized applications.
  • the electrochemical device may exploit the structural properties of the composite material that are derived primarily from continuous, oriented high-strength fiber reinforcement in a binding matrix to provide packaging while promoting processability and enhancing properties such as stiffness, and chemical and hygroscopic resistance.
  • Laminates may be designed to be isotropic or anisotropic, balanced or unbalanced, symmetric or asymmetric, depending on the in-use forces a component must withstand.
  • the electrochemical device may be incorporated into laminates making it possible to develop lightweight, complex shapes and to produce large parts with integral reinforcing members while providing additional functionality afforded by this invention.
  • Ingredients for composite materials that may be used with the electrochemical device include, but are not limited to: additives and modifiers, such as, ablatives, colorants, pigments, conductive fillers, coupling agents, decorative flakes, flame/smoke-suppressant additives, foaming agents, low-profile additives, styrene-suppressant additives, thickening agents, toughening agents, UV stabilizers, and viscosity control agents.
  • Adhesives include, but are not limited to: acrylic, bismaleimide, cyanoacrylate, epoxy, nylon, phenolic, polyimide, silicone, and urethane.
  • Casting resins include, but are not limited to: acrylic, epoxy, and unsaturated polyester.
  • Catalysts, promoters, and curing agents include, but are not limited to: cobalt naphthenate, amines, hardeners, initiators, and peroxides.
  • Coatings and sizings include, but are not limited to: conductive, decorative, electrostatic, EMI-attenuation, flame retardant, in-mold, paint, powder, and protective.
  • Compounds that may be used include, but are not limited to: bulk molding (BMC), fairing compounds (formerly paste systems), low-pressure molding, sheet molding (SMC), solid surface, thermoplastic, and thick molding.
  • Core materials and flow media include, but are not limited to: balsa, flow media for resin infusion, foam core, honeycomb, inorganic, expanding syntactic core, and nonexpanding syntactic core.
  • Fabrics that may be used include, but are not limited to: aramid, aramid/glass hybrid, C-glass, carbon, carbon/aramid hybrid, carbon/glass hybrid, ceramic, E-Glass, metallized, and structural high-strength glass (S- and R-type).
  • Inorganic fibers that may be used include, but are not limited to: aluminum, basalt, boron, C-Glass, ceramic, E-Glass, quartz, silicon carbide, and structural high-strength glass (S- and R-type).
  • Organic fibers that may be used include, but are not limited to: aramid, PAN-based carbon, pitch-based carbon, rayon-based carbon, hybrid commingled fibers, nylon, polybenzimidazole, polyester, polyethylene, and UHMW polyethylene (ultra-high molecular weight).
  • Fillers that may be used include, but are not limited to: alumina trihydrate, calcium carbonate, calcium sulfate, carbon black, gypsum, kaolin, mica, microspheres, milled glass fiber, nanophase (organic/inorganic), recyclate, silica, amorphous silica, talc, and wollastonite.
  • Gel coats that may be used include, but are not limited to: anti-fouling, chemical-/corrosion-resistant, conductive, fire-retardant, general-purpose, marine, potable-water grades, and UV-curable.
  • Matrix materials that may be used include, but are not limited to: ceramic and metallic.
  • Thermoplastic matrix resins that may be used include, but are not limited to: acetal, acrylonitrile butadiene styrene (ABS), liquid crystal polymer, methyl methacrylate, nylon (polyamide), PBT, polyamide-imide, polyarylene ketone, sulfide, polycarbonate, polyester (PET), polyether ketone family (PEK, PEKK, PEEK), polyetherimide, polyethersulfone, polyethylene, polyimide, polyphenylene sulfide (PPS), polypropylene, polyvinyl chloride, fluorinated polymers, polystyrene, styrene monomer (diluent), acrylonitrile, polybutylene terephthalate, polyphenylene oxide, polysulfone, polydimethylsiloxane, polyurethane, polyvinyl alcohol, PVDF, and polytetrafluoroethylene.
  • ABS acrylonitrile butad
  • Thermoset matrix resins that may be used include, but are not limited to: acrylic, bismaleimide, cyanate ester, epoxy, phenolic, polyimide, unsaturated polyester, urethane, UV-curable, and vinyl ester.
  • Unimpregnated preforms that may be used include, but are not limited to: aramid, carbon, ceramic, chopped fiber, continuous fiber, E-Glass, hybrid fiber, quartz, and structural high-strength glass (S- and R-type).
  • Thermoplastic prepregs that may be used include, but are not limited to: commingled/cowoven yarns, fabric, interlaced, mat, RTP sheet (GMT), tape, and tow or roving.
  • Thermoset prepregs that may be used include, but are not limited to: bismaleimide, cyanate ester, epoxy, phenolic, unsaturated polyester, polyimide, and vinyl ester.
  • Unimpregnated reinforcements that may be used include, but are not limited to: aramid, aramid/glass hybrid, C-glass, carbon, carbon/aramid hybrid, carbon/glass hybrid, ceramic, E-Glass, and structural high-strength glass (S- and R-type).
  • the electrochemical device is incorporated into neat thermoset or thermoplastic polymers without additional reinforcement using traditional thermoset or thermoplastic processing techniques, such as blow molding, injection molding, extrusion, thermoforming, vacuum forming, compression molding, etc.
  • the electrochemical device and panel composite integrates ballistic protection and energy functionality into a single component to reduce the mass that previously existed in the sum of the individual components.
  • the result is a multifunctional armor panel, as shown in Figure 6 , that produces higher specific energy and offers an opportunity to increase payload compared to conventional battery technologies.
  • the cell may be embedded within existing personal protective equipment suits.
  • a Nomex-based composite suit (coupled with an adhesive) will provide a suitable package for the battery; thus, providing battery and structural functionality.
  • the electrochemical device and panel composite may replace inert structural components and/or aerodynamic/hydrodynamic surfaces on Unmanned Air Vehicles (UAV), Unmanned Underwater Vehicles (UUV), and missile bodies while providing electrical power to the vehicle. Increasing the energy density can expand their range/payload capability.
  • UAV Unmanned Air Vehicles
  • UUV Unmanned Underwater Vehicles
  • missile bodies while providing electrical power to the vehicle. Increasing the energy density can expand their range/payload capability.
  • the electrochemical device and panel composite may be useful for other applications such as: aerospace applications, such as for fuselage, wings, wingbox, tail, empennage, ailerons, spoilers, composite inboard and outboard landing flaps, landing gear, rear spars, and fixed trailing edge assemblies, and interiors, such as seating, doors, floors, walls, aesthetic components, horizontal stabilizer, elevator and rudder, winglets, wing fixed trailing edge, wing-to-fuselage fairing, engine cowlings, engine pylons, pressure bulkhead, launch vehicles, fuel tanks, exploration instruments, satellites, space bases, and UAV airframes.
  • Automotive applications include, but are not limited to: body panels, structural components, under-the-hood parts, frames/chassis, and drive shafts.
  • Boating applications include, but are not limited to: yacht rigging systems (masts, shrouds, stays, and spreaders), hull, deck, and interior structure.
  • Civil infrastructure applications include, but are not limited to: bridges and bridge beams, decking, and enclosures.
  • Building construction applications include, but are not limited to: countertops, doors, window frames, bathtubs, and other home construction/remodeling materials, structural frame, cladding, roofing, siding, decking, emergency housing, truck trailers, outdoor signage, earthquake repair and upgrades/column wrap, manhole covers, trench covers, acoustic wall panels, marine piling, piers, residential wall panels, tanks, grating, platforms, and walkways.
  • Appliances and business equipment applications include, but are not limited to: handles, housing, and components.
  • Fuel cells applications include, but are not limited to: system components, such as bipolar plates, end plates, fuel tanks, and other system components.
  • Oil and gas applications include, but are not limited to: composite risers, deep-sea umbilical, and piping.
  • Sports and recreation applications include, but are not limited to: skis, fishing rods, tennis rackets, kayaks and paddles, windsurfing masts and boards, hockey sticks, bicycle components, and golf clubs and shafts.
  • Renewable energy applications include, but are not limited to: wind turbine blades, wave and tidal generator rotor blades.
  • Utility infrastructure applications include, but are not limited to: transmission towers, distribution poles and cross arms, battery boxes, casings, and telescoping portable antennas.
  • Example 1 Fabrication of a structural battery
  • a structural battery design consists of a Li-ion bi-cell that incorporates:
  • the outside anodes were cut from commercial stock, and the perimeter was cleaned using NMP to form the area for the perimeter seal.
  • two picture frame seals (with one extended side) were cut from 3 mil Suryln® film.
  • the picture frames were then heat sealed to the anodes.
  • Two pieces of Freya Energy safety separator modified by the manufacturer to improve adhesion and provide higher temperature tolerance were cut about 10 mm larger than the cathode.
  • a double sided commercial cathode was cut to shape with a terminal so it extends beyond the perimeter of the anode.
  • the cathode terminal was then coated with a high temperature polymer solution (PEI) and dried followed by an adhesion promoting layer of ethylene acrylic acid (EAA) and dried.
  • PEI high temperature polymer solution
  • EAA ethylene acrylic acid
  • the separator layers were then laminated to each side of the cathode.
  • the separator became bonded to cathode and to, each other beyond the perimeter of the electrode.
  • the excess separator was trimmed off leaving 1 to 3 mm around the perimeter of the cathode to insure complete encapuslation to prevent shorting.
  • the cell was then assembled by stacking the 3 layers together in careful alignment and heat sealing the three sides of the picture frame, leaving the fourth side with the extended Surlyn film open.
  • the cell was then activated by adding electrolyte through the open side.
  • the cell was ready to incorporate into a composite.
  • the battery has a high specific energy and it is fully bonded rather than a stack of loose individual layers.
  • the reason for this is that the cell is designed to be laminatable (with a suitable perimeter seal and laminatable separator). Outer packaging is not used; instead the foil current collectors serve as part or all of the outside packaging as shown in the cell design of Figure 4 and the image of Figure 5 .
  • the cell is very thin with thin foil current collectors (10-25 micron) that act as air and moisture barriers.
  • the bi-cell with two outside anodes and a double-sided cathode in between, which, doubles the capacity and increases the specific energy slightly.
  • the battery functionality and improved adhesion in the panels thereby creating a structural battery component that can be integrated into composite panels.
  • This battery can be integrated into a fiber-reinforced composite where the layers of the composite will provide both structure and battery packaging (including electrical isolation). Examples of reinforcements include carbon fiber and fiberglass.
  • the battery is 0.33 mm thick, has a nominal open circuit voltage of 3.7 V per cell, and has a 5.6 mAh/cm 2 cathode capacity. Assuming a 100 cm 2 cell active area, this equates to a 560 mAh cell capacity producing 2.072 Wh at a mass of 11 g. Therefore, the specific energy is 188.72 Wh/kg, and the areal energy density is 207.2 Wh/m 2 .
  • the gain in specific energy with this approach is significant. For example, a conventional battery of this scale weights approximately 4 g more, which means the specific energy would drop to approximately 136 Wh/kg.
  • the electrochemical device has an approximately 39% improvement in specific energy over a state-of-the-art Li-ion cell, assuming one could be procured at 0.33 mm thickness.
  • a structural battery design as shown in Figure 8 , consists of a Li-ion bi-cell electrochemical device (10) that incorporates:
  • the outside current collector was cut to size.
  • the current collector may be two pieces or one piece folded.
  • the cathode slurry was then patch coated by applying masking tape to the perimeter of the current collector and drawing down the slurry over the masked foil.
  • the cathodes were then dried.
  • Two pieces of special Freya Energy safety separator with improved adhesion and higher temperature tolerance were cut to size (about 10 mm larger than the anode).
  • a double sided anode or hand coated double sided anode was cut to shape.
  • a small soft copper tube was used for the terminal which extends beyond the perimeter of the cathode.
  • the anode terminal was then coated with a high temperature polymer solution (PEI or PAI) and dried.
  • PEI or PAI high temperature polymer solution
  • Tin adhesion promoting layer of acidified polypropylene was heat sealed to the tab.
  • the separator layers were then placed on each side of the anode and heat sealed around the perimeter. The excess separator was trimmed off beyond the heat seal leaving the seal around the perimeter of the anode insuring complete encapsulation to prevent shorting.
  • the cell was then assembled by stacking the 3 layers together in careful alignment. Two sides were ultrasonically welded. The third side with the anode tab was then ultrasonically welded with a formed horn that bridges the anode terminal which was bonded to the aluminum outer current collector by heat. The fourth side was left open for activation. The electrolyte was added through the open side and then the side was ultrasonically welded. The cell was subjected to formation to charge the cell.
  • Example 3 Fabrication of a curved battery
  • a curved structural battery design consists of a Li-ion bi-cell that incorporates:
  • the outside current collector was cut to size.
  • the current collector may be two pieces or one piece folded. If the current collected is folded, the folded edge cannot be along the curve edge.
  • the cathode slurry was then patch coated using a patterned screen (like silk screening) and drawing down the slurry over the screen. The cathodes were then dried and calendared. Two pieces of special Freya Energy safety separator with improved adhesion and higher temperature tolerance were cut to size (about 10 mm larger than the anode).
  • a double sided anode was made by cutting a copper coated non-woven current collector to size and attaching a small soft copper tube for the terminal using a conductive adhesive.
  • the non-woven current collector was then dip coated in the anode slurry coating to saturate the non-woven and give the desired weight.
  • the anode was then dried and calendered.
  • the anode terminal was coated with a high temperature polymer solution (PEI or PAI) and dried, followed by heat sealing an adhesion promoting layer of acidified polypropylene to the tab.
  • the separator layers were then placed on each side of the anode and heat sealed around the perimeter. The excess separator was trimmed off beyond the heat seal leaving the seal around the perimeter of the anode insuring complete encapsulation to prevent shorting.
  • the cell was then assembled by stacking the 3 layers together in careful alignment.
  • the cell does not comprise a folded cathode
  • one of the straight sides is ultrasonically welded.
  • the assembly was then formed over a round or contoured anvil and the two curved sides are welded - either stepwise with a static unit continuously using an ultrasonic seamer.
  • the side with the anode tab is treated as described in Example 1.
  • the fourth side was left open for activation.
  • the electrolyte was added through the open side and then the side is ultrasonically welded.
  • the cell was subjected to formation to charge the cell.
  • the cell now had a permanent curvature to it and was ready to incorporate into a curved composite (such as the housing of a missile or torpedo).
  • a urethane mixture prepolymer, polyols, and catalyst components was metered as a liquid from a casting machine on top of the armor plate.
  • Ballistic testing was conducted in accordance with the provisions of MIL-STD-662F, dated 18 December 1997, using caliber .30-06 Springfield, 166 grain, AP, M2 ammunition.
  • the test samples were mounted on an indoor range, 25.0 feet from the muzzle of a test barrel to produce zero degree obliquity impacts.
  • Velocity screens were positioned at 10.0 and 20.0 feet, that in conjunction with elapsed time counters (chronographs), were used to compute projectile velocities 15.0 feet from the muzzle.
  • Penetrations were determined by visual examination of a 0.020 inch thick aluminum alloy 2024T3 witness panel positioned 6.0 inches behind, and parallel to, the test samples.

Description

    CROSS REFERENCE TO RELATED APPLICATIONS BACKGROUND
  • Today's highly mobile world is very dependent upon portable power and portable power today is trending towards electric rather than gasoline, which means batteries or other electrochemical devices are the primary power source. The energy needed for many devices and applications leads to the batteries consuming a significant portion of the mass and volume allocated to the device, and also imposes significant constraints on the shape and size of the device. For example, a large portion of the mass of a laptop computer is contained in the battery, and the shape is fixed by the shape of the battery.
  • Because of the space and weight taken up by batteries, engineers often try to have batteries serve multiple purposes. For example, the lead acid batteries in forklifts serve as ballast for stability. There are however, more instances where added weight and or volume are not beneficial. In these cases, engineers would like to get electrochemical devices to provide additional functions besides power. There are many applications where "multi-functional" composites containing energy storage would find application. As batteries take up space, one of the most obvious approaches is to have them contribute to the mechanical aspects of the structure. As most batteries are delivered in cases, it is technically feasible to try to gain structural aspects from fastening them together. However, this after-the-fact approach is not optimal.
  • There have been efforts in the past to use the carbon fiber in composites as anode material for lithium ion batteries and turn the composite into a battery. However, due to numerous problems with the composite resin, the carbon mat thickness, the need for vapor barriers and electrolytes, the efforts were never commercially successful. A much more direct approach is to embed individual lithium ion cells into a composite or polymer.
  • Unmanned Arial Vehicles (UAVs), and especially Micro UAVs that have electric propulsion are excellent examples which are critically dependent on weight and where composite structural panels are common. Accordingly, there is interest in using advanced multi-functional composites. Bending modulus is critical to UAV panels and the mechanics of bending are well understood. Consumer electronics are additional examples that are dependent on mass and volume. Accordingly, it is desirable to use multi-functional cells in the structure of these devices to reduce the mass and volume associated with the power supply without reducing the capacity or safety.
    WO 2010/062391 A2 pertains to a high energy density bicell battery being constructed from positive and negative electrodes, with a layer separating the two electrodes, and polymer packaging heat-sealed around the electrode assemblies.
    From EP 1 359 633 A1 a galvanic cell is known that comprises thin electrodes sealed in plastic foils which are partly metallized on sides forming an electrical contact with the electrode on one side and an external flag on the other side.
    US 2010/190047 A1 discloses a stacked energy storage device having at least two cell segments arranged in a stack. In particular, each cell segment has a first electrode unit having a first active material electrode, a second electrode unit having a second active material electrode, and an electrolyte layer between the active material electrodes.
    JP 2007 066806 A pertains to a bipolar battery that has a single cell comprising a cathode active layer, an electrolyte layer and an anode active layer. The single cell is arranged between a pair of current collectors and a flexible armoring material in which a sealing part is arranged to seal the single cell.
  • BRIEF SUMMARY
  • An electrochemical device comprises one or more anode, cathode, and separator. In addition it has two or more current collectors. In some embodiments, the separator is also an electrolyte. The anode and cathode are between the two current collectors and each is adhered to an adjacent current collector. The separator is between the anode and cathode and adhered to the anode and cathode. The current collectors are a barrier, and are sealed together to create a sealed container for the anode, cathode, and separator. The electrochemical device may be integrated into a composite or polymer panel suitable for uses such as structural load bearing panels or sheets for aircraft wings or fuselage, composite armor, unmanned underwater vehicle, torpedo, missile body, consumer electronics, etc. The electrochemical device may include, but is not limited to, energy storage (batteries, supercapacitors), and energy generation (fuel cells).
  • These and other objects and advantages shall be made apparent from the accompanying drawings and the description thereof.
  • BRIEF DESCRIPTION OF THE FIGURES
  • The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments, and together with the general description given above, and the detailed description of the embodiments given below, serve to explain the principles of the present disclosure.
    • FIGURE 1 is a schematic drawing of an embodiment of an electrochemical device.
    • FIGURE 2 is a schematic drawing of an embodiment of an electrochemical device.
    • FIGURE 3 is a top view of four cells connected in series ready to be embedded in composite.
    • FIGURE 4 is a drawing an embodiment of a battery showing an expanded Bi-cell assembly.
    • FIGURE 5 is a photograph of an embodiment of a battery showing the Cu foil current collector / outside packaging.
    • FIGURE 6 is a top and side view of an embodiment of a multifunctional composite armor design.
    • FIGURE 7 is a graph of charge/ discharge curves and specific capacities of an embodiment of an electrochemical device and a control battery.
    • FIGURE 8 is a schematic drawing of an embodiment of an electrochemical device.
    • FIGURE 9 is photographs of an embodiment of an electrochemical device integrated into an armor panel.
    • FIGURE 10 is photographs of an embodiment of an electrochemical device integrated into an armor panel after ballistic tests.
    DETAILED DESCRIPTION
  • There is a need to provide improved energy storage technologies for a variety of applications, where the storage device is: thinner, lighter with higher energy, power, or both per unit mass and volume (specific energy and density), can conform to a variety of surface shapes, and can withstand mechanical loads. The device may be a battery, supercapacitor, a combination of both, or other electrochemical device.
  • A multilayer electrochemical device embedded within a composite or polymer panel possesses both the mechanical attributes necessary to carry shear stress, thus contributing to the bending modulus and increased energy density for any given chemistry. The electrochemical device may use various battery chemistries or super capacitor chemistries. Panels containing these devices can be made with various three dimensional structures which can provide structural support. Thin structures can withstand some degree of flexing. The devices may be used in a variety of structural panels subjected to stresses for many applications. The outside layer metal current collectors act as the packaging for the electrochemical device, and all the inner layers of the electrochemical device, including the current collectors, the anode(s) and cathode(s) and the separator(s) are adhered together so as not to provide a slip plane that would compromise the strength of the panel.
  • An electrochemical device (10) comprises one or more anode (11), cathode (12), and separator (13). In some embodiments, the separator (13) is also an electrolyte. In addition it has two or more current collectors (14). The anode (11) and cathode (12) are between the two current collectors (14) and each is adhered to an adjacent current collector (14). The separator (13) is between the anode (11) and cathode (12) and adhered to the anode (11) and cathode (11). The current collectors (14) are a barrier against leakage of the electrolyte and against moisture and oxygen. They are sealed together to create a sealed container for the one or more anode (11), cathode (12), and separator (13), either by a polymeric layer between them or directly by welding. In some embodiments, as shown in Figure 1, the device (10) additionally comprises a perimeter seal (15). The perimeter seal (15) is bonded between the two outer current collectors (14), and the combination of outer current collectors (14) and perimeter seal (15) act to create the sealed container for the one or more anode (11), cathode (12), and separator (13).
  • In some embodiments, the electrochemical device comprises two or more anodes, cathodes, or both. The anodes or cathodes may be double-sided, which is an electrode attached to a current collector, such as in the middle of the electrode layer. A separator layer is on both sides of the double-sided electrode, and the opposite electrode is adjacent to the separator layer on both sides. In some embodiments, the device comprises at least one double-sided cathode. In some embodiments, the device comprises at least one double-sided anode.
  • In some embodiments, the anode may be for a lithium ion electrochemical device. Examples of anodes include, but are not limited to carbon, lithium titanate, silicon, tin, and others. The anode should be pin hole free. In some embodiments, the anode may be for a NiMH (nickel metal hydride) electrochemical device. Examples of anodes include, but are not limited to hydrogen-absorbing metal alloys. In some embodiments, the anode may be for a supercapacitor. Examples of anodes include, but are not limited to high surface area carbon, metal oxides, and nitrides. In some embodiments, the anode may be for a lead acid electrochemical device. Examples of anodes include, but are not limited to lead, lead compounds such as lead sulfate, carbon, and lead-carbon mixtures. In some embodiments, the anode may be for a Li-S (lithium sulfur) electrochemical device. Other anodes are well known in the art. In some embodiments, the thickness of the anode is from about anode 1 to about 100 microns, such as about 10 to about 80 microns, about 20 to about 70 microns, about 25 to about 60 microns, and about 20 to about 40 microns.
  • In some embodiments, the cathode may be for a lithium ion electrochemical device. Examples of cathodes include, but are not limited to lithium cobalt oxide, nickel cobalt aluminum oxide, manganese oxide, manganese spinel, nickel-manganese-cobalt oxide, nickel-manganese oxide, lithium iron phosphate, lithium cobalt phosphate, lithium manganese phosphate, and derivatives, and sulfur. In some embodiments, the cathode may be for a NiMH (nickel metal hydride) electrochemical device. Examples of cathodes include, but are not limited to nickel hydroxyl and oxyhydroxy compounds. In some embodiments, the cathode may be for a supercapacitor. Examples of cathodes include, but are not limited to high surface area carbon, metal oxides, and nitrides. In some embodiments, the supercapacitor cathode has the same composition as the anode, or may have a different composition. In some embodiments, the cathode may be for a lead acid electrochemical device. Examples of cathodes include, but are not limited to lead sulfate, and lead oxide. In some embodiments, the cathode may be for a Li-S (lithium sulfur) electrochemical device. Other cathodes are well known in the art. In some embodiments, the thickness of the cathode is from about 1 to about 200 microns, such as about 10 to about 150 microns, about 25 to about 120 microns, and about 50 to about 100 microns, and about 60 to about 80 microns.
  • The current collector may be for an anode or cathode. The outer current collectors act as a barrier, which prevents the passage of electrolyte, oxygen and water. In some embodiments, the current collector acts as a mass transport barrier. Examples of current collectors for anodes include copper, aluminum, nickel, and stainless steel. Aluminum current collectors may be useful for both the anode and cathode if the cell voltage is about 3 volts or less. In some embodiments, the outer current collectors are a solid foil and of sufficient thickness so as not to have pinholes. In some embodiments, the outer current collectors are very thin, such as about 5 to about 50 microns, about 10 to about 30 microns, about 10 to about 25 microns, or about 15 to about 20 microns. In some embodiments, the inner current collectors are very thin, such as about 5 to about 50 microns, about 10 to about 30 microns, about 10 to about 25 microns, or about 15 to about 20 microns. The current collectors are electrochemically stable to the voltages of the cell and preferably exhibit low resistance. They are of sufficient strength to be processed and preferably can bend around rolls for continuous processing. The external current collectors are pinhole free to provide the barrier properties and of at least minimal strength to prevent damage during processing and integration into a composite. The surface should provide good wetting and bonding to the resin of the composite. Examples of current collectors for cathodes include aluminum and stainless steel. In some embodiments, the current collector may be nickel.
  • A current collector may be embedded within an anode or cathode (double-sided anode or cathode) if it is not the outer layer of the electrochemical device. A current collector within an anode or cathode need not be a solid foil, it may selected from expanded metals, carbon nonwoven webs, and metal coated carbon non-woven webs and metal coated non-woven polymer webs. In some embodiments, all the cathodes are electrically connected together in parallel, such as by connecting all the current collectors attached to the cathodes, and all the anodes are electrically connected together in parallel, such as by connecting all the current collectors attached to the anodes. In some embodiments, the electrodes are connected serially.
  • In some embodiments, the outer current collectors are bonded or adhered to the adjacent electrode. In some embodiments, the outer current collectors are each independently bonded or adhered to anodes. In some embodiments, the outer current collectors are each independently bonded or adhered to cathodes. The outer current collectors are prepared by one of several methods. The electrode material may be "patch" coated onto the current collector. Patch coating involves applying coating to only a portion of the current collector, such as leaving the perimeter clean so that the perimeter may be sealed to the other outer current collector. Patch coating can be achieved by intermittent coating by a reverse roll or similar coater, a screen coater/printer, printing, gravure coating, ink jet printing, or any other application technique that permits uncoated areas. Another method is to apply a continuous coating and then clean off the areas to seal. A third way is to mask the area to be left uncoated. It may be beneficial to use a primer between the current collector and the electrode to increase adhesion and/or improve performance as is well known in the art.
  • In some embodiments, where the outer current collectors are of the same polarity, the outer current collectors can be welded together. They are fully welded together with the exception of a passage for the alternate terminal. This can be accomplished by ultrasonic welding, laser welding, or a pulsed DC welder with a contact wheel known as a rotary seamer. When welded together, the outer current collectors provide a very good barrier. They are sealed hermetically. However, even when sealed, the current collectors allow the opposite electrode to exit the device without making an electrical connection to the opposite electrode.
  • In some embodiments, the electrochemical device additionally comprises a perimeter seal. In some embodiments, the perimeter seal is also a barrier to oxygen, or moisture, and a barrier to the electrolyte. In some embodiments, the perimeter seal is used as an electrical insulator to prevent an electrical connection between the two outer current collectors. The perimeter seal is stable in the presence of the electrolytes and may help to carry stress. The current collector may be treated beforehand to enhance the sealing to the perimeter seal. Examples of perimeter seals include: ionomer resins (such as Surlyn®), ethylene acrylic acid (EAA), polyolefin, acidified polyolefin, polyvinylidene difluoride (PVDF), polyimide, polyamide, epoxy, and polyurethane, and other polymeric material that bonds well to metal foils and is inert to the electrolyte. In some embodiments, the separator is bonded to the perimeter seal. A perimeter seal is bonded to the outer current collectors, and acts as a barrier to moisture, oxygen, or both, and prevents the migration of the electrolyte. Transmission through the seal is dependent upon the seal width and cross-section. A thinner and/or wider seal minimizes migration. The films prior to sealing are in the range of about 10 to about 150 microns, such as about 25 to about 125 microns, about 30 to about 110 microns, or about 50 to about 100 microns. In some embodiments, the perimeter seal is applied as a coating. The perimeter seal is able to withstand the buildup of internal pressure (up to about 2 atmospheres) and temperatures of at least 130°C.
  • The separator is an electrical insulator that allows the electrolyte to conduct ions without conducting electrons. In some embodiments, the separator is also an electrolyte. In some embodiments, an adhesive layer is applied to the separator to adhere the anode and the cathode to the separator. Examples of separators include microporous polyolefin, a ceramic coated polyethylene terephthalate (PET), and PVDF. In some embodiments, the separator is coated with an adhesive layer selected from poly(vinylidene fluoride-co-hexafluoropropylene) (PVDF-HFP) copolymer, chlorinated polypropylene, and maleic anhydride/polypropylene. In some embodiments, the separator is a polymer selected from polyimides and polyamides, wherein the polymer is interdispersed with at least one adhesive resin, such as modified polypropylene, to form a separator with intrinsic adhesive characteristics. In some embodiments, the separator is a polymer selected from crosslinked PVDF and crosslinked poly(ethylene oxide) (PEO).
  • In some embodiments, the adhesive layers are thermally activated, the adhesive is activated, and the separator bonds the electrodes together after the electrolyte has been added and allowed to migrate into the separator and electrodes. A low melting point adhesive resin (such as about 80 to about 85[deg.]C) can be used that does not damage the electrolyte, but bonds all the layers together with heat and pressure.
  • In some embodiments, the separator is from about 5 to about 250 microns in thickness, such as from about 10 to about 100 microns, and about 10 to about 50 microns. To allow the electrolyte to conduct ions, the separator has void space. In some embodiments the separator is from about 10% to about 90% void, such as from about 20% to about 80%), about 30% to about 80%, about 40% to about 70%, and from about 45%) to about 65%>. The voids in the separator are in the form of interconnected pores. The average size of the pores in the separator range from about 30 nm to 10 microns, such as from about 40 nm to about 7 microns, about 50 nm to about 5 microns, and from about 100 nm to about 2 microns.
  • In some embodiments, the separator (13) is wrapped around an electrode and sealed around it. The separator (13) is effectively formed into a bag or pouch like structure and an electrode is enclosed inside the separator (13), as shown in Figure 2. The outer current collectors (14) are sealed together to form a perimeter seal (15). This helps to prevent shorting. In some embodiments, the electrode is double-sided. When the device is fabricated, an electrode enclosed in a separator (13) is placed on top of an electrode of the opposite polarity, and a second electrode of the opposite polarity is placed on top of the enclosed electrode.
  • The electrolyte used in the electrochemical device depends on the nature of the anode and cathode. The electrolyte may be a liquid or solid. For lithium-ion batteries, the electrolyte may be a mixture of carbonates or other high dielectric solvents with a lithium containing salt, such as L1CO3, LiPF 6, LiAs 4, LiB0 4, lithium bis(oxalate)borate (LiBOB), and triflate. Examples of solvents include ethylene carbonate (EC), diethyl carbonate (DEC), dimethyl carbonate (DMC), ethylmethyl carbonate (EMC), propylene carbonate (PC), [gamma]-butyrolactone, as well as special additives such as vinyl ethylene carbonate (VEC), fluoro ethylene carbonate (FEC), and methyl acetate (MA). The concentration of the salts is optimized to the system, but is generally in the range of 1 molar. In other embodiments, the electrolyte may be an ionic liquid. For NiMH cells, the electrolyte may be an aqueous alkaline solution, such as potassium hydroxide. For lead acid batteries, the electrolyte is an aqueous acidic solution.
  • In some embodiments, electrochemical device may also comprise a supercapacitor. In these devices, the electrolyte may be either an aqueous or nonaqueous solvent containing a salt or other ionic species.
  • A structural panel may be made comprising the electrochemical device. The panel and the electrochemical device provide a structural support. Because the electrochemical device is a solid mass and can transmit stress and does not compress or slip it does not weaken or significantly weaken the panel it is part of.
  • In one embodiment the electrochemical device can then be assembled into panels by embedding one or more in a mosaic structure as shown in Figure 3, within a composite. In some embodiments the composite comprises a thin glass fiber (or other suitable material) / epoxy (or other suitable material) layer on each side. The composite adhesively bonds to the outer current collector metal surfaces of the electrochemical device and provides protection to the outer current collectors. The cells can easily be arranged and wired in series connections to provide conventional voltages of 14V, 28V, or even higher voltages within a single panel. The mosaic structure offers further benefits of creating a honeycomb like continuous phase. The size of the electrochemical devices can be adjusted to optimize different objectives. Very large electrochemical devices can be used to maximize specific energy, or a mosaic of smaller cells can be used to provide redundancy in case an electrochemical device is damaged (by enemy fire or other events).
  • In some embodiments, the panel is planar, or has a simple (single directional) curve. It can be thin or ultrathin which provides a much higher specific energy for the form factor. This structural integrity is a necessary element of producing a curved cell that will retain its shape. Using the outside current collector layer metals as the packaging of the cell eliminates the non-contributing weight of the pouch packaging. The panel material becomes the battery package, which bonds to the metal surfaces of the foils during processing and protects the cells from physical damage. In some embodiments, the panel material is a composite selected from carbon fiber and fiberglass. In some embodiments, the majority of the outer surface of the electrochemical device is encased in the polymer. In some embodiments, the electrochemical device and panel are curved.
  • Fabrication
  • The individual electrochemical devices may be laid up as a two-dimensional tiled array within the composite. The gaps between the single electrochemical devices of a multi-cell battery will also allow for adhesive bonding between successive layers of composite materials, or will allow the polymeric panel material to fill the gaps. The design can employ large numbers of individual electrochemical devices in parallel and in series to provide higher total capacity as well as higher voltages. Further the multi-electrochemical device two-dimensional array design provides a high level of redundancy where if one electrochemical device is damaged, the remainder of the electrochemical devices will still function.
  • The layers in the electrochemical device are fully bonded rather than a stack of loose individual layers. Outer packaging is not needed for the electrochemical device; instead the current collectors serve as part or all of the packaging, as shown in the cell design of Figure 4 and the image of Figure 5.
  • The electrochemical device, as it is a laminated structure, can be easily fabricated in a simple curved structure as well a flat panel. The device must have the appropriate dimensions for the curvature and must be fabricated in or near the final shape. Complex contours are possible by pre-forming the foils.
  • In one embodiment, the outer current collector forms one terminal, which may be either copper or aluminum foil, may have a tab for the opposite electrode coming though the sealed outer current collectors, or the perimeter seal on one side. The device can be structured with copper foil on one side and aluminum (positive terminal) on the other. The cells can then be assembled into panels by embedding them in a composite or polymer with a thin composite or resin layer on each side as shown in Figures 3 and 4.
  • The electrochemical device may be incorporated into a variety of fabrication methods, such as hand layup, resin transfer molding, vacuum assisted resin transfer molding, resin film infusion, filament winding, pultrusion, etc., thereby creating complex 3D multifunctional structures (including sandwich constructions, which combine a lightweight core material with laminated composite skins). Adhesion of the electrochemical device within the panel prevents it from behaving as a defect or a void by allowing the matrix to bond to the metal foils. In some embodiments, the outer current collectors are treated before cell assembly to enhance the adhesion between the resin and the current collector. Methods to enhance adhesion include mechanically or chemically roughening the outer surface of the current collectors to increase surface area, or applying a tie coating such as a silane to the outer surface of the current collector.
  • Properties
  • This composite integrates structural and energy functionality into a single component to eliminate the redundancies of parasitic mass that previously existed in the sum of the individual components. The result is a multifunctional composite panel that produces a 39% or greater increase in specific energy compared to standard batteries containing the same chemistry, and offers an opportunity to increase payload, operational lifetime, safety, or function compared to state-of-the art battery technologies.
  • In some embodiments the electrochemical device is a Li-ion bi-cell that comprises a bonded microporous polymeric separator, copper foil current collectors (about 10 microns thick), aluminum foil current collectors (about 15 microns thick), and liquid EC/EMC electrolyte. In some embodiments, the electrochemical device has two outside anodes and a double-sided cathode. Such an electrochemical device may be 0.33 mm thick, have a nominal open circuit voltage of 3.7 V per cell, and a 5.6 mAh/cm2 cathode capacity (2.8mAh/cm2 per side). Assuming a 100 cm2 cell active area, this equates to a 560 mAh cell capacity producing 2.072 Wh at a mass of 11 g. Therefore, the specific energy is 188.72 Wh/kg, and the areal energy density is 207.2 Wh/m2. Assuming the hull of a vehicle has a usable surface area of 10 m2, the result would be total energy storage of 2,072 Wh for a vehicle.
  • The gain in specific energy for this size device is significant. For example, a conventional cell and packaging of this scale weights approximately 4 g more, which means the specific energy would drop to approximately 136 Wh/kg. The electrochemical device has an approximately 39% improvement in specific energy over a state-of-the-art Li-ion cell, assuming one could be procured at 0.33 mm thickness.
  • The electrochemical devices may be fabricated into a composite at either 95°C or 130°C. An upper limit of 130°C allows this technology to be embedded into ultra high molecular weight polyethylene (UHMWPE), such as Dyneema® and Spectra Shield®, or fiberglass composites, such as HJ1, during consolidation. The Freya Energy safety separator (developed by Freya Energy Inc, Melbourne FL, www.freyaenergy.com to provide improved safety in lithium ion cells), was modified by Freya Energy by increasing the percentage bonding resin and changing the thermal protection resin to increase the adhesive bond strength and increase the temperature tolerance for the composite fabrication. Processing pressures are not an issue for the cells as they are designed to withstand 68947 kPa (10,000 psi) hydrostatic pressure; therefore, they should withstand typical composite processing pressures.
  • In some embodiments, an electrochemical device has multiple electrodes, which together to give a thicker, higher capacity, and higher specific energy device. This is especially useful where the bending modulus is more important than strength (such as in an airfoil) as the thicker device adds thickness to the composite panel. A thicker device also facilitates the use of non-woven current collectors in the inner electrodes further increasing specific energy and energy density.
  • Supercapacitor
  • In some embodiments, the electrochemical device is a supercapacitor, or a battery hybridized with a supercapacitor. For a supercapacitor device that has an anode and cathode material with overall density of about 2g/cm3, the electrolyte has a density of about 1g/cm3, and the anode and cathode material will have a capacitance of about 200F/g, the capacitance of the system is about 0.2F (because the electrodes are in series). Assuming electrode thickness of 10 microns and a voltage of 1.5V across the electrodes (asymmetric configuration), the areal energy density is: E cm 2 = 1 2 CV 2 = 0.225 J cm 2 = 0.625 Wh / m 2
    Figure imgb0001
  • If a vehicle has usable surface area of 10 m2, then there can be a total energy storage of 6.25 Wh due to the supercapacitor alone, for a single layer device with a thickness 70 microns. If multiple layers are formed, the areal energy density will increase. With 20 layers (approaching 1mm thick), the energy density would be 12.5 Wh/m2.
  • Considering the power of the system, if the total energy stored for a single layer of 6.25 Wh, a 5-second discharge of this energy would provide average power of 4,500 W. With a discharge time of 1 second, this would equate to 22,500 W from the single layer. Multiple layers would act to increase this more than linearly.
  • Table 1 shows a breakdown of the attributes of an electrochemical battery and supercapacitor.
    Figure imgb0002
  • Composites overview
  • Beyond high strength and low weight, composite materials can offer a multitude of other properties such as good vibrational damping and low coefficient of thermal expansion. These characteristics may be modified to allow them to be engineered for specialized applications.
  • The electrochemical device may exploit the structural properties of the composite material that are derived primarily from continuous, oriented high-strength fiber reinforcement in a binding matrix to provide packaging while promoting processability and enhancing properties such as stiffness, and chemical and hygroscopic resistance. Laminates may be designed to be isotropic or anisotropic, balanced or unbalanced, symmetric or asymmetric, depending on the in-use forces a component must withstand. The electrochemical device may be incorporated into laminates making it possible to develop lightweight, complex shapes and to produce large parts with integral reinforcing members while providing additional functionality afforded by this invention.
  • Ingredients for composite materials that may be used with the electrochemical device include, but are not limited to: additives and modifiers, such as, ablatives, colorants, pigments, conductive fillers, coupling agents, decorative flakes, flame/smoke-suppressant additives, foaming agents, low-profile additives, styrene-suppressant additives, thickening agents, toughening agents, UV stabilizers, and viscosity control agents. Adhesives include, but are not limited to: acrylic, bismaleimide, cyanoacrylate, epoxy, nylon, phenolic, polyimide, silicone, and urethane. Casting resins include, but are not limited to: acrylic, epoxy, and unsaturated polyester. Catalysts, promoters, and curing agents include, but are not limited to: cobalt naphthenate, amines, hardeners, initiators, and peroxides. Coatings and sizings include, but are not limited to: conductive, decorative, electrostatic, EMI-attenuation, flame retardant, in-mold, paint, powder, and protective. Compounds that may be used include, but are not limited to: bulk molding (BMC), fairing compounds (formerly paste systems), low-pressure molding, sheet molding (SMC), solid surface, thermoplastic, and thick molding. Core materials and flow media include, but are not limited to: balsa, flow media for resin infusion, foam core, honeycomb, inorganic, expanding syntactic core, and nonexpanding syntactic core. Fabrics that may be used include, but are not limited to: aramid, aramid/glass hybrid, C-glass, carbon, carbon/aramid hybrid, carbon/glass hybrid, ceramic, E-Glass, metallized, and structural high-strength glass (S- and R-type). Inorganic fibers that may be used include, but are not limited to: aluminum, basalt, boron, C-Glass, ceramic, E-Glass, quartz, silicon carbide, and structural high-strength glass (S- and R-type). Organic fibers that may be used include, but are not limited to: aramid, PAN-based carbon, pitch-based carbon, rayon-based carbon, hybrid commingled fibers, nylon, polybenzimidazole, polyester, polyethylene, and UHMW polyethylene (ultra-high molecular weight). Fillers that may be used include, but are not limited to: alumina trihydrate, calcium carbonate, calcium sulfate, carbon black, gypsum, kaolin, mica, microspheres, milled glass fiber, nanophase (organic/inorganic), recyclate, silica, amorphous silica, talc, and wollastonite. Gel coats that may be used include, but are not limited to: anti-fouling, chemical-/corrosion-resistant, conductive, fire-retardant, general-purpose, marine, potable-water grades, and UV-curable. Matrix materials that may be used include, but are not limited to: ceramic and metallic. Thermoplastic matrix resins that may be used include, but are not limited to: acetal, acrylonitrile butadiene styrene (ABS), liquid crystal polymer, methyl methacrylate, nylon (polyamide), PBT, polyamide-imide, polyarylene ketone, sulfide, polycarbonate, polyester (PET), polyether ketone family (PEK, PEKK, PEEK), polyetherimide, polyethersulfone, polyethylene, polyimide, polyphenylene sulfide (PPS), polypropylene, polyvinyl chloride, fluorinated polymers, polystyrene, styrene monomer (diluent), acrylonitrile, polybutylene terephthalate, polyphenylene oxide, polysulfone, polydimethylsiloxane, polyurethane, polyvinyl alcohol, PVDF, and polytetrafluoroethylene. Thermoset matrix resins that may be used include, but are not limited to: acrylic, bismaleimide, cyanate ester, epoxy, phenolic, polyimide, unsaturated polyester, urethane, UV-curable, and vinyl ester. Unimpregnated preforms that may be used include, but are not limited to: aramid, carbon, ceramic, chopped fiber, continuous fiber, E-Glass, hybrid fiber, quartz, and structural high-strength glass (S- and R-type). Thermoplastic prepregs that may be used include, but are not limited to: commingled/cowoven yarns, fabric, interlaced, mat, RTP sheet (GMT), tape, and tow or roving. Thermoset prepregs that may be used include, but are not limited to: bismaleimide, cyanate ester, epoxy, phenolic, unsaturated polyester, polyimide, and vinyl ester. Unimpregnated reinforcements that may be used include, but are not limited to: aramid, aramid/glass hybrid, C-glass, carbon, carbon/aramid hybrid, carbon/glass hybrid, ceramic, E-Glass, and structural high-strength glass (S- and R-type). In some embodiments, the electrochemical device is incorporated into neat thermoset or thermoplastic polymers without additional reinforcement using traditional thermoset or thermoplastic processing techniques, such as blow molding, injection molding, extrusion, thermoforming, vacuum forming, compression molding, etc.
  • Product Applications
  • The electrochemical device and panel composite integrates ballistic protection and energy functionality into a single component to reduce the mass that previously existed in the sum of the individual components. The result is a multifunctional armor panel, as shown in Figure 6, that produces higher specific energy and offers an opportunity to increase payload compared to conventional battery technologies.
  • Further, the cell may be embedded within existing personal protective equipment suits. For example, a Nomex-based composite suit (coupled with an adhesive) will provide a suitable package for the battery; thus, providing battery and structural functionality.
  • Additionally, the electrochemical device and panel composite may replace inert structural components and/or aerodynamic/hydrodynamic surfaces on Unmanned Air Vehicles (UAV), Unmanned Underwater Vehicles (UUV), and missile bodies while providing electrical power to the vehicle. Increasing the energy density can expand their range/payload capability.
  • The electrochemical device and panel composite may be useful for other applications such as: aerospace applications, such as for fuselage, wings, wingbox, tail, empennage, ailerons, spoilers, composite inboard and outboard landing flaps, landing gear, rear spars, and fixed trailing edge assemblies, and interiors, such as seating, doors, floors, walls, aesthetic components, horizontal stabilizer, elevator and rudder, winglets, wing fixed trailing edge, wing-to-fuselage fairing, engine cowlings, engine pylons, pressure bulkhead, launch vehicles, fuel tanks, exploration instruments, satellites, space bases, and UAV airframes. Automotive applications include, but are not limited to: body panels, structural components, under-the-hood parts, frames/chassis, and drive shafts. Boating applications include, but are not limited to: yacht rigging systems (masts, shrouds, stays, and spreaders), hull, deck, and interior structure. Civil infrastructure applications include, but are not limited to: bridges and bridge beams, decking, and enclosures. Building construction applications include, but are not limited to: countertops, doors, window frames, bathtubs, and other home construction/remodeling materials, structural frame, cladding, roofing, siding, decking, emergency housing, truck trailers, outdoor signage, earthquake repair and upgrades/column wrap, manhole covers, trench covers, acoustic wall panels, marine piling, piers, residential wall panels, tanks, grating, platforms, and walkways. Appliances and business equipment applications include, but are not limited to: handles, housing, and components. Fuel cells applications include, but are not limited to: system components, such as bipolar plates, end plates, fuel tanks, and other system components. Oil and gas applications include, but are not limited to: composite risers, deep-sea umbilical, and piping. Sports and recreation applications include, but are not limited to: skis, fishing rods, tennis rackets, kayaks and paddles, windsurfing masts and boards, hockey sticks, bicycle components, and golf clubs and shafts. Renewable energy applications include, but are not limited to: wind turbine blades, wave and tidal generator rotor blades. Utility infrastructure applications include, but are not limited to: transmission towers, distribution poles and cross arms, battery boxes, casings, and telescoping portable antennas.
  • EXAMPLES Example 1: Fabrication of a structural battery
  • A structural battery design consists of a Li-ion bi-cell that incorporates:
    • Two - bonded microporous polymeric separators
    • Two outer single sided anodes with 10 micron copper foil current collector
    • One double sided cathode with 15 micron aluminum foil current collector
    • Liquid LiPF6/mixed carbonate electrolyte absorbed into the electrodes and separator.
  • The outside anodes were cut from commercial stock, and the perimeter was cleaned using NMP to form the area for the perimeter seal. Next, two picture frame seals (with one extended side) were cut from 3 mil Suryln® film. The picture frames were then heat sealed to the anodes. Two pieces of Freya Energy safety separator modified by the manufacturer to improve adhesion and provide higher temperature tolerance were cut about 10 mm larger than the cathode. A double sided commercial cathode was cut to shape with a terminal so it extends beyond the perimeter of the anode. The cathode terminal was then coated with a high temperature polymer solution (PEI) and dried followed by an adhesion promoting layer of ethylene acrylic acid (EAA) and dried. The separator layers were then laminated to each side of the cathode. The separator became bonded to cathode and to, each other beyond the perimeter of the electrode. The excess separator was trimmed off leaving 1 to 3 mm around the perimeter of the cathode to insure complete encapuslation to prevent shorting. The cell was then assembled by stacking the 3 layers together in careful alignment and heat sealing the three sides of the picture frame, leaving the fourth side with the extended Surlyn film open. The cell was then activated by adding electrolyte through the open side. The cell was subjected to formation to charge the cell. After formation, the cell was degassed and the entire cell bonded together by heating the cell to about 90°C and putting the cell under moderate pressure 103-689 kPa (=15-100 psi)). The cell was ready to incorporate into a composite.
  • The battery has a high specific energy and it is fully bonded rather than a stack of loose individual layers. The reason for this is that the cell is designed to be laminatable (with a suitable perimeter seal and laminatable separator). Outer packaging is not used; instead the foil current collectors serve as part or all of the outside packaging as shown in the cell design of Figure 4 and the image of Figure 5. The cell is very thin with thin foil current collectors (10-25 micron) that act as air and moisture barriers. The bi-cell with two outside anodes and a double-sided cathode in between, which, doubles the capacity and increases the specific energy slightly. The battery functionality and improved adhesion in the panels thereby creating a structural battery component that can be integrated into composite panels. This battery can be integrated into a fiber-reinforced composite where the layers of the composite will provide both structure and battery packaging (including electrical isolation). Examples of reinforcements include carbon fiber and fiberglass.
  • The battery is 0.33 mm thick, has a nominal open circuit voltage of 3.7 V per cell, and has a 5.6 mAh/cm2 cathode capacity. Assuming a 100 cm2 cell active area, this equates to a 560 mAh cell capacity producing 2.072 Wh at a mass of 11 g. Therefore, the specific energy is 188.72 Wh/kg, and the areal energy density is 207.2 Wh/m2. The gain in specific energy with this approach is significant. For example, a conventional battery of this scale weights approximately 4 g more, which means the specific energy would drop to approximately 136 Wh/kg. The electrochemical device has an approximately 39% improvement in specific energy over a state-of-the-art Li-ion cell, assuming one could be procured at 0.33 mm thickness.
  • Multiple single-cell battery components were fabricated and subjected to electrochemical characterization and testing to evaluate electrochemical functionality (e.g. charge/discharge curves). The batteries produced higher specific energy and energy density compared to state-of-the-art battery technologies, as shown by the data in Figure 7. This figure compares a control cell (built using a commercial separator and standard flexible pouch packaging) to the new batteries. As seen in the graph in Figure 7, the new cell cycle comparably to the control cell, as seen by the cell voltage. The specific capacities of the new cells demonstrate an increase in specific energy of approximately 20%. This increase in specific energy means 20% more power without any additional weight.
  • Examples 2 Fabrication of structural cell with perimeter welded outer current collectors.
  • A structural battery design, as shown in Figure 8, consists of a Li-ion bi-cell electrochemical device (10) that incorporates:
    • Two - bondable microporous polymeric separators (13)
    • Two outer single sided cathode (12) with 25 micron aluminum foil current collector (14)
    • One double sided anode (11) with 10 micron copper foil current collector (16)
    • Liquid LiPF6/mixed carbonate electrolyte absorbed into the electrodes and separator.
    • A welded seam perimeter seal (15)
  • The outside current collector was cut to size. The current collector may be two pieces or one piece folded. The cathode slurry was then patch coated by applying masking tape to the perimeter of the current collector and drawing down the slurry over the masked foil. The cathodes were then dried. Two pieces of special Freya Energy safety separator with improved adhesion and higher temperature tolerance were cut to size (about 10 mm larger than the anode). A double sided anode or hand coated double sided anode was cut to shape. A small soft copper tube was used for the terminal which extends beyond the perimeter of the cathode. The anode terminal was then coated with a high temperature polymer solution (PEI or PAI) and dried. Tin adhesion promoting layer of acidified polypropylene was heat sealed to the tab. The separator layers were then placed on each side of the anode and heat sealed around the perimeter. The excess separator was trimmed off beyond the heat seal leaving the seal around the perimeter of the anode insuring complete encapsulation to prevent shorting. The cell was then assembled by stacking the 3 layers together in careful alignment. Two sides were ultrasonically welded. The third side with the anode tab was then ultrasonically welded with a formed horn that bridges the anode terminal which was bonded to the aluminum outer current collector by heat. The fourth side was left open for activation. The electrolyte was added through the open side and then the side was ultrasonically welded. The cell was subjected to formation to charge the cell. After formation, the cell was degassed through the anode terminal, which was then ultrasonically sealed and the entire cell was bonded together by heating the cell to about 90[deg.]C and putting the cell under moderate pressure (103-689 kPa (=15-100 psi)). The cell was now ready to incorporate into a composite.
  • Example 3: Fabrication of a curved battery
  • A curved structural battery design consists of a Li-ion bi-cell that incorporates:
    • Two - bondable microporous polymeric separators
    • Two outer single sided cathodes with 25 micron aluminum foil current collectors
    • One double sided anode with a copper coated non-woven current collector
    • Liquid LiPF6/mixed carbonate electrolyte absorbed into the electrodes and separator.
  • The outside current collector was cut to size. The current collector may be two pieces or one piece folded. If the current collected is folded, the folded edge cannot be along the curve edge. The cathode slurry was then patch coated using a patterned screen (like silk screening) and drawing down the slurry over the screen. The cathodes were then dried and calendared. Two pieces of special Freya Energy safety separator with improved adhesion and higher temperature tolerance were cut to size (about 10 mm larger than the anode). A double sided anode was made by cutting a copper coated non-woven current collector to size and attaching a small soft copper tube for the terminal using a conductive adhesive. The non-woven current collector was then dip coated in the anode slurry coating to saturate the non-woven and give the desired weight. The anode was then dried and calendered. The anode terminal was coated with a high temperature polymer solution (PEI or PAI) and dried, followed by heat sealing an adhesion promoting layer of acidified polypropylene to the tab. The separator layers were then placed on each side of the anode and heat sealed around the perimeter. The excess separator was trimmed off beyond the heat seal leaving the seal around the perimeter of the anode insuring complete encapsulation to prevent shorting. The cell was then assembled by stacking the 3 layers together in careful alignment. If the cell does not comprise a folded cathode, one of the straight sides is ultrasonically welded. The assembly was then formed over a round or contoured anvil and the two curved sides are welded - either stepwise with a static unit continuously using an ultrasonic seamer. (The side with the anode tab is treated as described in Example 1. The fourth side was left open for activation. The electrolyte was added through the open side and then the side is ultrasonically welded. The cell was subjected to formation to charge the cell. After formation, the cell was degassed through the anode terminal, which was then ultrasonically sealed and the entire cell was bonded together using a contoured press heated to about 90°C and putting the cell under moderate pressure (103-689 kPa (=15-100 psi)) for sufficient time for the entire cell to come to a uniform temperature. The cell now had a permanent curvature to it and was ready to incorporate into a curved composite (such as the housing of a missile or torpedo).
  • Example 4: Composite Armor Panel Fabrication
  • A cast urethane process with a mold of dimensions roughly 16.5mm x 50cm x 50cm was used to fabricate a multifunctional composite armor panel. A steel armor plate (6.35mm x 50cm x 50cm MIL-A-46100, High Hard (HH)) was placed in the mold. A urethane mixture (prepolymer, polyols, and catalyst components) was metered as a liquid from a casting machine on top of the armor plate. A single layer of Vectran® (liquid crystal polyester-polyarylate) fabric was placed on top of the first casting of urethane. Alternating layers of urethane and Vectran® fabric were laid up in the mold until 32 layers of a Vectran®/urethane composite backing system was built up to achieve roughly 10 mm of a spall liner composite adhesively bonded to the HH steel armor plate. Prior to the last layer of fabric, on the backside of each armor panel, 4 electrochemical devices from example 1 were placed in the composite and molded into place.
  • Slits were cut into the last layer of fabric to allow for the tabs of the batteries to come through for interconnection. These tabs were wrapped in paper and taped down on the fabric so that no urethane could bond to them during processing and their integrity would not be compromised. The lid was placed on the assembly and clamped down to evacuate all of the excess urethane material. The clamping force was sufficient to force the extra urethane in and between all layers of the composite armor panel, and up and out of the mold. The mold temperature was maintained at about 93 °C during and after the process to ensure proper pre-cure of the material prior to demolding the part. The armor panel was demolded after approximately 20-30 minutes and subsequently post-cured at temperatures between about 93 °C to 121 °C for approximately 12 to 36 hours to ensure completion of the chemical reaction and attainment of material properties.
  • An example of this integrated product is shown in Figure 9.
  • Example 5: Composite Armor Panel Ballistics Testing
  • Ballistic testing was conducted in accordance with the provisions of MIL-STD-662F, dated 18 December 1997, using caliber .30-06 Springfield, 166 grain, AP, M2 ammunition. The test samples were mounted on an indoor range, 25.0 feet from the muzzle of a test barrel to produce zero degree obliquity impacts. Velocity screens were positioned at 10.0 and 20.0 feet, that in conjunction with elapsed time counters (chronographs), were used to compute projectile velocities 15.0 feet from the muzzle. Penetrations were determined by visual examination of a 0.020 inch thick aluminum alloy 2024T3 witness panel positioned 6.0 inches behind, and parallel to, the test samples.
  • The results showed a V50 Ballistic Limit (BL) of 2020 fps (2017 fps high partial, 1981 fps low partial) for the base armor panel without the batteries and a V50 BL of 2143 fps (2238 fps high partial, 2035 fps low partial) for the panels with the batteries, indicating the integration of the batteries did not degrade ballistic performance.
  • The post-test images are shown in Figure 10, where it can be seen that even though the shots penetrated the batteries, there were no signs of fire or other safety issues during testing.

Claims (15)

  1. An electrochemical device comprising one or more anode, cathode, and separator; and two or more current collectors;
    wherein the anode and cathode are between the two current collectors and each is adhered to an adjacent current collector, and the separator is between the anode and cathode and adhered to the anode and cathode;
    wherein the current collectors are a barrier against moisture and/ or oxygen; and characterized in that the current collectors are bonded together to create a sealed container for the anode, cathode, and separator; preferably wherein the outer anodes or cathodes are the current collectors.
  2. The electrochemical device of claim 1, wherein the device is hermetically sealed inside the current collectors.
  3. The electrochemical device of either one of claim 1 or 2, additionally comprising a perimeter seal, wherein the perimeter seal is bonded between the two current collectors.
  4. The electrochemical device of any one of the preceding claims, wherein the device comprises two or more anodes, cathodes, or both.
  5. The electrochemical device of any one of the preceding claims, wherein at least one electrode is double-sided; preferably wherein the double-sided electrode is wrapped in a separator which is sealed around the electrode.
  6. The electrochemical device of any one of the preceding claims, wherein all the cathodes are electrically connected and all the anodes are electrically connected.
  7. The electrochemical device of any one of the preceding claims, wherein the perimeter seal is selected from ionomer resin, ethylene acrylic acid (EAA), polyolefin, acidified polyolefin, polyvinylidene difluoride (PVDF), polyimide, polyamide, epoxy, and polyurethane.
  8. The electrochemical device of any one of the preceding claims, wherein the separator is selected from a microporous polyolefin, a ceramic coated polyethylene terephthalate (PET), and a PVDF separator; the separator is coated with an adhesive layer selected from poly(vinylidene fluoride-co-hexafluoropropylene) (PVDF-HFP) copolymer, chlorinated polypropylene, and maleic anhydride/polypropylene; preferably wherein the separator is a polymer selected from polyimides and polyamides, wherein the polymer is interdispersed with at least one adhesive; more preferably wherein the separator is a polymer selected from crosslinked PVDF and crosslinked poly(ethylene oxide) (PEO).
  9. The electrochemical device of any one of the preceding claims, wherein the separator is from 10 µm (=10 micron) to 50 µm (=50 micron) in thickness.
  10. The electrochemical device of any one of the preceding claims, wherein the size of the pores in the separator range from 30nm to 10 µm (=10 micron).
  11. A structural panel comprising the electrochemical device of any one of the preceding claims; preferably wherein the panel comprises a polymer, and the outer current collectors of the electrochemical device are adhesively bonded to the polymer.
  12. The structural panel of claim 11, wherein the panel comprises a composite of resin and reinforcement.
  13. The structural panel of any one of claims 11 to 12, wherein a majority of the outer surface of the electrochemical device is encased in the polymer.
  14. The structural panel of any one of claims 11 to 13, wherein the electrochemical device and panel are conformed to a surface contour.
  15. A method for making an electrochemical device according to claim 1, comprising the steps of:
    providing one or more electrolyte, and separator; and two or more current collectors and electrodes; wherein at least one electrode is an anode and one electrode is a cathode;
    the device is assembled by stacking a current collector, anode, separator, cathode, and a second current collector;
    the electrolyte is added to the separator; and
    stack is laminated by heating to 90°C or higher under at least 103 kPa (=15 psi) of pressure.
EP13795889.8A 2012-05-08 2013-05-08 Multifunctional cell for structural applications Active EP2852990B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261643947P 2012-05-08 2012-05-08
PCT/US2013/040149 WO2014021970A2 (en) 2012-05-08 2013-05-08 Multifunctional cell for structural applications

Publications (2)

Publication Number Publication Date
EP2852990A2 EP2852990A2 (en) 2015-04-01
EP2852990B1 true EP2852990B1 (en) 2018-01-31

Family

ID=49667546

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13795889.8A Active EP2852990B1 (en) 2012-05-08 2013-05-08 Multifunctional cell for structural applications

Country Status (5)

Country Link
US (1) US9520580B2 (en)
EP (1) EP2852990B1 (en)
JP (1) JP6220865B2 (en)
KR (1) KR101984203B1 (en)
WO (1) WO2014021970A2 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020102661A1 (en) * 2018-11-15 2020-05-22 ZAF Energy Systems, Incorporated Alkaline pouch cell with coated terminals
DE102020129659A1 (en) 2020-11-11 2022-05-12 Airbus Operations Gmbh Integrated actuator element with electroactive polymer
DE102021100713A1 (en) 2021-01-15 2022-07-21 Airbus Operations Gmbh Structural component for a vehicle
DE102021101976A1 (en) 2021-01-28 2022-07-28 Airbus Operations Gmbh Structural component for a vehicle
EP4040635A1 (en) 2021-02-08 2022-08-10 Airbus Operations GmbH Structural component of an automobile and fixing attachment
DE102021104928A1 (en) 2021-03-02 2022-09-08 Airbus Operations Gmbh Passenger service unit for a passenger cabin of an aircraft or spacecraft
EP4216337A1 (en) 2022-01-20 2023-07-26 Airbus Operations GmbH Structural battery for a vehicle

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2505166B (en) * 2012-08-03 2018-04-04 Bae Systems Plc Component including a structural supercapacitor
US10121607B2 (en) * 2013-08-22 2018-11-06 Corning Incorporated Ceramic separator for ultracapacitors
CN105637705B (en) * 2013-10-16 2019-04-19 Agc株式会社 Power supply structure, window are with resin plate body and its manufacturing method
US9660470B2 (en) 2014-09-08 2017-05-23 Nokia Technologies Oy Flexible, hybrid energy generating and storage power cell
DE102014113588A1 (en) * 2014-09-19 2016-03-24 Manz Ag Method for producing a battery cell
WO2016106016A1 (en) * 2014-12-24 2016-06-30 3M Innovative Properties Company Porous adhesive networks in electrochemical devices
GB2537935B (en) 2015-05-01 2021-02-24 Intelligent Energy Ltd Aerial vehicle
WO2017079025A1 (en) * 2015-11-02 2017-05-11 Rutgers, The State University Of New Jersey Electrochemical cell having thin metal foil packaging and a method for making same
US10414358B2 (en) 2016-02-03 2019-09-17 The Boeing Company Composite panel power system
US11289769B2 (en) 2016-03-03 2022-03-29 Apple Inc. Binders for wet and dry lamination of battery cells
CN108780864B (en) * 2016-03-03 2021-08-20 苹果公司 Binder for wet-laminated and dry-laminated battery cells
US10868337B2 (en) 2016-03-08 2020-12-15 Beijing Hawaga Power Storage Technology Company Ltd Cell-core for lithium slurry battery, and lithium slurry battery module
CN107681114B (en) * 2016-08-01 2020-08-14 北京好风光储能技术有限公司 Positive plate, preparation process and lithium slurry battery containing positive plate
CN107681115B (en) * 2016-08-01 2020-08-04 北京好风光储能技术有限公司 Negative plate of lithium slurry battery
EP3222514B1 (en) * 2016-03-21 2019-05-22 Airbus Operations GmbH Skin panel with an energy-storing layer for an aircraft or spacecraft and method for manufacturing an energy-storing layer for a skin panel
US10147557B2 (en) 2016-09-13 2018-12-04 The Mitre Corporation Enhanced structural supercapacitors
US10522874B2 (en) * 2016-11-01 2019-12-31 The Boeing Company Solid state fiber-based battery system and method of forming same
EP3336948B1 (en) * 2016-12-14 2019-09-11 Airbus Operations GmbH Method for tailoring and integrating a fuel cell unit into a vehicle
US11233276B2 (en) 2017-04-07 2022-01-25 Beijing Hawaga Power Storage Technology Company Ltd. Lithium slurry battery system
TWI822676B (en) 2017-04-18 2023-11-21 英商立可行有限公司 Energy storage device
WO2019055893A1 (en) * 2017-09-18 2019-03-21 Avx Corporation Ultracapacitor with a low leakage current
US10934013B2 (en) 2017-09-22 2021-03-02 The Boeing Company Aircraft fuselage apparatus having embedded structural batteries
TWI676315B (en) * 2017-10-20 2019-11-01 輝能科技股份有限公司 Composite battery cell
CN108461285B (en) * 2017-12-29 2023-07-11 安徽瀚宇电气有限公司 Buffer type bulge-preventing self-healing locomotive capacitor
US10991935B2 (en) 2018-03-27 2021-04-27 The Mitre Corporation Structural lithium-ion batteries with carbon fiber electrodes
WO2020099351A1 (en) * 2018-11-12 2020-05-22 Fischer Eco Solutions Gmbh Method for bonding two plates together for a fuel cell, especially gluing bipolar plates in a fuel cell
DE102019218979A1 (en) 2019-12-05 2021-06-10 Airbus Operations Gmbh Lightweight structure for a vehicle and an aircraft
KR20210075773A (en) * 2019-12-13 2021-06-23 현대자동차주식회사 Vehicle body member having charger and discharger function
KR20210109730A (en) * 2020-02-27 2021-09-07 현대자동차주식회사 Vehicle body member having charger and discharger function
CN111504141A (en) * 2020-03-31 2020-08-07 江苏厚生新能源科技有限公司 Application of high-energy-density lithium ion battery in torpedo
US11511527B2 (en) 2020-04-14 2022-11-29 Saint-Gobain Performance Plastics Corporation Composite film
KR102447927B1 (en) * 2020-08-20 2022-09-28 한국과학기술원 Laminated Structural Battery with High Battery Performances
DE102020133854A1 (en) 2020-12-16 2022-06-23 Airbus Operations Gmbh Structural composite laminate for an aircraft component, aircraft component made therewith and aircraft
US11705601B2 (en) 2021-08-18 2023-07-18 Lockheed Martin Corporation Structural battery for an aircraft vehicle
CN113782820B (en) * 2021-11-11 2022-03-15 深圳市兴禾自动化股份有限公司 Pole piece and pole piece bag coincide electric core
CN113782839B (en) * 2021-11-11 2022-03-25 深圳市兴禾自动化股份有限公司 Online pole piece bag making and laminating process and bag making and laminating production line thereof
CN113782838B (en) * 2021-11-11 2022-03-15 深圳市兴禾自动化股份有限公司 Cell thermal compounding manufacturing process
US20230327255A1 (en) * 2022-04-06 2023-10-12 Meta Platforms Technologies, Llc High capacity curved battery cells
CN116864864A (en) * 2023-08-23 2023-10-10 河南宸硕新能源科技有限公司 Energy-saving heating device and heating method for lithium battery pack

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5940470A (en) * 1982-08-30 1984-03-06 Fuji Elelctrochem Co Ltd Laminated cell
JPS5972374A (en) * 1982-10-20 1984-04-24 国産金属工業株式会社 Lock apparatus
JPS60184265U (en) * 1984-05-17 1985-12-06 カシオ計算機株式会社 thin battery
JPH01239761A (en) * 1988-03-18 1989-09-25 Hitachi Maxell Ltd Thin lithium battery
JPH01239759A (en) * 1988-03-18 1989-09-25 Hitachi Maxell Ltd Thin lithium battery
JPH02112149A (en) * 1988-10-20 1990-04-24 Hitachi Maxell Ltd Thin lithium battery
JP3270175B2 (en) * 1992-04-15 2002-04-02 日本電気株式会社 Electric double layer capacitor
JPH08167415A (en) * 1994-12-14 1996-06-25 Sanyo Electric Co Ltd Thin type high polymer solid electrolyte battery and its manufacture
JP3544106B2 (en) * 1997-09-29 2004-07-21 株式会社ユアサコーポレーション Thin non-aqueous electrolyte battery
JP2000048781A (en) 1998-07-28 2000-02-18 Ricoh Co Ltd Flat, thin battery
WO2002015300A1 (en) 2000-08-10 2002-02-21 University Of Virginia Patent Foundation Multifunctional battery and method of making the same
US6805946B2 (en) 2000-12-04 2004-10-19 Advanced Ceramics Research, Inc. Multi-functional composite structures
US7063917B2 (en) 2001-02-21 2006-06-20 Ahlstrom Mount Holly Springs, Llc Laminated battery separator material
JP2003151558A (en) * 2001-11-14 2003-05-23 Matsushita Electric Ind Co Ltd Non-aqueous electrolyte secondary battery
DE10219424A1 (en) * 2002-05-02 2003-11-20 Varta Microbattery Gmbh Galvanic element with thin electrodes
US7318984B2 (en) 2002-05-17 2008-01-15 Nitto Denko Corporation Adhesive composition-supporting separator for battery and electrode/separator laminate obtained by using the same
US7267908B2 (en) * 2004-08-30 2007-09-11 Toyota Technical Center Usa, Inc. In cycling stability of Li-ion battery with molten salt electrolyte
JP2006269295A (en) * 2005-03-24 2006-10-05 Ngk Spark Plug Co Ltd Thin battery and its manufacturing method
US20070015021A1 (en) * 2005-07-18 2007-01-18 Yaron Shrim Canless bi-cell
JP4720384B2 (en) * 2005-09-01 2011-07-13 日産自動車株式会社 Bipolar battery
GB0519807D0 (en) 2005-09-28 2005-11-09 Welding Inst Fuel cell assembly
US7855017B1 (en) 2005-11-09 2010-12-21 The United States Of America As Represented By The Secretary Of The Army Structural batteries and components thereof
US20080268341A1 (en) * 2007-03-14 2008-10-30 Teck Cominco Metals Ltd. High power batteries and electrochemical cells and methods of making same
US20090202903A1 (en) 2007-05-25 2009-08-13 Massachusetts Institute Of Technology Batteries and electrodes for use thereof
GB0823260D0 (en) 2008-12-20 2009-01-28 Qinetiq Ltd Multi-functional composite
CN102341949A (en) * 2009-01-27 2012-02-01 G4协同学公司 Variable volume containment for energy storage devices
HUE037809T2 (en) 2009-03-09 2018-09-28 Asahi Chemical Ind Polyolefin microporous membrane
WO2011098795A1 (en) 2010-02-09 2011-08-18 Bae Systems Plc Component including a rechargeable battery
KR101217562B1 (en) 2010-11-16 2013-01-02 삼성전자주식회사 Flexible battery and flexible electronic device including the same

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020102661A1 (en) * 2018-11-15 2020-05-22 ZAF Energy Systems, Incorporated Alkaline pouch cell with coated terminals
DE102020129659A1 (en) 2020-11-11 2022-05-12 Airbus Operations Gmbh Integrated actuator element with electroactive polymer
DE102021100713A1 (en) 2021-01-15 2022-07-21 Airbus Operations Gmbh Structural component for a vehicle
DE102021101976A1 (en) 2021-01-28 2022-07-28 Airbus Operations Gmbh Structural component for a vehicle
EP4040635A1 (en) 2021-02-08 2022-08-10 Airbus Operations GmbH Structural component of an automobile and fixing attachment
DE102021102901A1 (en) 2021-02-08 2022-08-11 Airbus Operations Gmbh Structural component for a vehicle and fastening arrangement
DE102021104928A1 (en) 2021-03-02 2022-09-08 Airbus Operations Gmbh Passenger service unit for a passenger cabin of an aircraft or spacecraft
EP4216337A1 (en) 2022-01-20 2023-07-26 Airbus Operations GmbH Structural battery for a vehicle

Also Published As

Publication number Publication date
WO2014021970A3 (en) 2014-04-03
JP2015520923A (en) 2015-07-23
KR101984203B1 (en) 2019-05-30
WO2014021970A2 (en) 2014-02-06
KR20150013249A (en) 2015-02-04
US9520580B2 (en) 2016-12-13
EP2852990A2 (en) 2015-04-01
JP6220865B2 (en) 2017-10-25
US20150093629A1 (en) 2015-04-02

Similar Documents

Publication Publication Date Title
EP2852990B1 (en) Multifunctional cell for structural applications
Galos et al. Energy storage structural composites with integrated lithium‐ion batteries: a review
KR101286827B1 (en) Electrode and production method thereof
US20130209839A1 (en) Component including a rechargeable battery
JP5386900B2 (en) Bipolar Lithium Ion Secondary Battery Current Collector Containing Organic Structure
AU2011214121B2 (en) Component including a rechargeable battery
US11855273B2 (en) Structural lithium-ion batteries with carbon fiber electrodes
CN105051961A (en) Non-aqueous electrolyte secondary battery
US20150044572A1 (en) Electrical energy storage structures
US11322810B2 (en) Jacketing of structural batteries
CN105103340A (en) Non-aqueous electrolyte secondary battery
JP6738164B2 (en) Exterior material for power storage device and power storage device
KR101772446B1 (en) High Stiffness Fiber Woven Fabric Based Structural Battery Composites
EP2765629A1 (en) Separator with heat-resistant insulating layer
US10439248B2 (en) Sandwich panels with battery cores
CN107204406A (en) Electrical storage device housing material and electrical storage device
KR101896413B1 (en) Energy storage structure and battery for energy storage structure
CN101030632B (en) Secondary battery set enhanced with glass fiber reinforced resin and its manufacture
EP2862216B1 (en) Structural composite battery with fluidic port for electrolyte
CN105074999A (en) Nonaqueous electrolyte secondary battery
Qidwai et al. Design and fabrication of multifunctional structure-power composites for marine applications
Thomas et al. Multifunctional Structure-Battery Composites for Marine Applications
KR20230102562A (en) Packaging material for battery and secondary battery including the same

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20141208

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAX Request for extension of the european patent (deleted)
REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602013032699

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: H01M0002020000

Ipc: H01M0002080000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RIC1 Information provided on ipc code assigned before grant

Ipc: H01G 11/82 20130101ALI20170615BHEP

Ipc: H01M 10/058 20100101ALN20170615BHEP

Ipc: H01G 11/52 20130101ALI20170615BHEP

Ipc: H01G 11/72 20130101ALI20170615BHEP

Ipc: H01G 11/80 20130101ALI20170615BHEP

Ipc: H01M 10/04 20060101ALI20170615BHEP

Ipc: H01M 10/12 20060101ALN20170615BHEP

Ipc: H01M 2/02 20060101ALI20170615BHEP

Ipc: H01M 10/052 20100101ALN20170615BHEP

Ipc: H01M 2/16 20060101ALI20170615BHEP

Ipc: H01G 11/76 20130101ALI20170615BHEP

Ipc: H01M 2/08 20060101AFI20170615BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: H01G 11/76 20130101ALI20170621BHEP

Ipc: H01G 11/82 20130101ALI20170621BHEP

Ipc: H01M 10/052 20100101ALN20170621BHEP

Ipc: H01G 11/52 20130101ALI20170621BHEP

Ipc: H01M 2/08 20060101AFI20170621BHEP

Ipc: H01M 10/058 20100101ALN20170621BHEP

Ipc: H01M 10/12 20060101ALN20170621BHEP

Ipc: H01M 2/02 20060101ALI20170621BHEP

Ipc: H01G 11/72 20130101ALI20170621BHEP

Ipc: H01M 10/04 20060101ALI20170621BHEP

Ipc: H01G 11/80 20130101ALI20170621BHEP

Ipc: H01M 2/16 20060101ALI20170621BHEP

INTG Intention to grant announced

Effective date: 20170706

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 968115

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180215

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602013032699

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 6

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180131

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 968115

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180430

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180430

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180531

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180501

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602013032699

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

26N No opposition filed

Effective date: 20181102

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180531

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180508

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180508

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180508

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20130508

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180131

Ref country code: MK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180131

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602013032699

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: H01M0002080000

Ipc: H01M0050183000

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230523

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20230412

Year of fee payment: 11

Ref country code: DE

Payment date: 20230412

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20230412

Year of fee payment: 11